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Catenoid limits of singly periodic minimal surfaces with Scherk-type ends

Hao Chen Institute of Mathematical Sciences, ShanghaiTech University, 201210 Pudong, Shanghai, China chenhao5@shanghaitech.edu.cn Peter Connor Department of Mathematical Sciences, Indiana University South Bend pconnor@iusb.edu  and  Kevin Li School of Science, Engineering, and Technology, Penn State Harrisburg khl3@psu.edu
Abstract.

We construct families of embedded, singly periodic minimal surfaces of any genus gg in the quotient with any even number 2n>22n>2 of almost parallel Scherk ends. A surface in such a family looks like nn parallel planes connected by n1+gn-1+g small catenoid necks. In the limit, the family converges to an nn-sheeted vertical plane with n1+gn-1+g singular points termed nodes in the quotient. For the nodes to open up into catenoid necks, their locations must satisfy a set of balance equations whose solutions are given by the roots of Stieltjes polynomials.

Key words and phrases:
minimal surfaces, saddle towers, node opening
2010 Mathematics Subject Classification:
Primary 53A10
H. Chen was partially supported by Individual Research Grant from Deutsche Forschungsgemeinschaft within the project “Defects in Triply Periodic Minimal Surfaces”, Projektnummer 398759432.

The goal of this paper is to construct families of singly periodic minimal surfaces (SPMSs) of any genus in the quotient with any even number 2n>22n>2 of Scherk ends (asymptotic to vertical planes). Each family is parameterized by a small positive real number τ>0\tau>0. In the limit τ0\tau\to 0, the Scherk ends tend to be parallel, and the surface converges to an nn-sheeted vertical plane with singular points termed nodes. As τ\tau increases, the nodes open up into catenoid necks, and the surface looks like parallel planes connected by these catenoid necks.

There are many previously known examples of such SPMSs. Scherk [Sch35] discovered the examples with genus zero and four Scherk ends, in 1835. Karcher [Kar88] generalized Scherk’s surface in 1988 with any even number 2n>22n>2 of Scherk ends. In this paper, examples of genus 0 will be called “Karcher–Scherk saddle towers” or simply “saddle towers”, and saddle towers with four Scherk ends will be called “Scherk saddle towers”. Karcher also added handles between adjacent pairs of ends, producing SPMSs of genus nn with 2n2n Scherk ends. Traizet glued Scherk saddle towers into SPMSs of genus (n23n+2)/2(n^{2}-3n+2)/2 with 2n>22n>2 Scherk ends because he was desingularizing simple arrangements of n>1n>1 vertical planes. In 2006, Martín and Ramos Batista [MRB06] replaced the ends of Costa surface by Scherk ends, thereby constructed an embedded SPMS of genus one with six Scherk ends and, for the first time, without any horizontal symmetry plane. Hauswirth, Morabito, and Rodríguez [HMR09] generalized this result in 2009, using an end-to-end gluing method to replace the ends of Costa–Hoffman–Meeks surfaces by Scherk ends, thereby constructed SPMSs of higher genus with six Scherk ends. In 2010, da Silva and Ramos Batista [dSRB10] constructed a SPMS of genus two with eight Scherk ends based on Costa surface. Also, Hancco, Lobos, and Ramos Batista [HLB14] constructed SPMSs with genus 2n2n and 2n2n Scherk ends in 2014.

The examples of da Silva and Ramos Batista as well as all examples of Traizet admit catenoid limits that can be constructed using techniques in the present paper.

One motivation of this work is an ongoing project that addresses to various technical details in the gluing constructions.

Roughly speaking, given any “graph” GG that embeds in the plane and minimizes the length functional, one could desingularize G×G\times\mathbb{R} into a SPMS by placing a saddle tower at each vertex. Previously, this was only proved for simple graphs under the assumption of an horizontal reflection plane [Tra96, Tra01]. Recently, we managed to allow the graph to have parallel edges, to remove the horizontal reflection plane by Dehn twist [CT21], and to prove embeddedness by analysing the bendings of Scherk ends [Che21].

However, we still require that the vertices of GG are neither “degenerate” nor “special”. Here, a vertex of degree 2k2k is said to be degenerate (resp. special) if kk (resp. k1k-1) of its adjacent edges extend in the same direction while other kk (resp. k1k-1) edges extend in the opposite direction. This limitation is due to the fact that a saddle tower with 2k2k Scherk ends can not have k1k-1 ends extending in the same direction while other k1k-1 ends extending in the opposite direction. Therefore, it is not possible to place a saddle tower at a degenerate or special vertex.

Nevertheless, we do know SPMSs that desingularize G×G\times\mathbb{R} where GG is a graph with degenerate vertex. To include these in the gluing construction, we need to place catenoid limits of saddle towers, as those constructed in this paper, at degenerate vertices. From this point of view, the present paper can be seen as preparatory: The insight gained here will help us to glue saddle towers with catenoid limits of saddle towers in a future project.

This paper reproduces the main result of the thesis of the third named author [Li12]. Technically, the construction implemented in [Li12] was in the spirit of [Tra02b], which defines the Gauss map and the Riemann surface at the same time, and the period of the surface was assumed horizontal. Here, for the convenience of future applications, we present a construction in the spirit of [Tra08, CT21, Che21], which defines all three Weierstrass integrands by prescribing their periods, and the period of the surface is assumed vertical. In particular, we will reveal that a balance condition in [Li12] is actually a disguise of the balance of Scherk ends: The unit vectors in the directions of the ends sum up to zero.

Acknowledgements

We would like to thank the referee for many helpful comments.

1. Main result

1.1. Configuration

We consider L+1L+1 vertical planes, L1L\geq 1, labeled by integers l[1,L+1]l\in[1,L+1]. Up to horizontal rotations, we assume that these planes are all parallel to the xzxz-plane, which we identify to the complex plane \mathbb{C}, with the xx-axis (resp. zz-axis) corresponding to the real (resp. imaginary) axis. We use the term “layer” for the space between two adjacent parallel planes. So there are LL layers.

We want nl1n_{l}\geq 1 catenoid necks on layer ll, i.e. between the planes ll and l+1l+1, 1lL1\leq l\leq L. For convenience, we adopt the convention that nl=0n_{l}=0 if l<1l<1 or l>Ll>L, and write N=nlN=\sum n_{l} for the total number of necks. Each neck is labeled by a pair (l,k)(l,k), where 1lL1\leq l\leq L and 1knl1\leq k\leq n_{l}.

To each neck is associated a complex number ql,k×={0}q_{l,k}\in\mathbb{C}^{\times}=\mathbb{C}\setminus\{0\}, 1lL1\leq l\leq L, 1knl1\leq k\leq n_{l}. Then the positions of the necks are prescribed at lnql,k+2mπi\ln q_{l,k}+2m\pi{\rm i}, mm\in\mathbb{Z}. Recall that the zz-axis is identified to the imaginary axis of the complex plane \mathbb{C}, so the necks are periodic with period vector (0,0,2π)(0,0,2\pi). Note that, if we multiply ql,kq_{l,k}’s by the same complex factor cc, then the necks are all translated by lnc(mod2πi)\ln c\pmod{2\pi{\rm i}}. So we may quotient out translations by fixing q1,1=1q_{1,1}=1.

Moreover, each plane has two ends asymptotic to vertical planes. We label the end of plane ll that expands in the x-x (resp. xx) direction by 0l0_{l} (resp. l\infty_{l}). To be compatible with the language of graph theory that were used for gluing saddle towers [CT21], we use

𝖧={ηl:1lL+1,η{0,}}\mathsf{H}=\{\eta_{l}\colon 1\leq l\leq L+1,\eta\in\{0,\infty\}\}

to denote the set of ends. When 0l0_{l} is used as subscript for parameter xx, we write xl,0x_{l,0} instead of x0lx_{0_{l}} to ease the notation; the same applies to l\infty_{l}.

To each end is associated a real number θ˙h\dot{\theta}_{h}, h𝖧h\in\mathsf{H}. They prescribe infinitesimal changes of the directions of the ends. More precisely, for small τ\tau, we want the unit vector in the direction of the end hh to have a yy-component or the order τθ˙h+𝒪(τ2)\tau\dot{\theta}_{h}+\mathcal{O}(\tau^{2}).

Remark 1.

Multiplying θ˙\dot{\theta} by a common real constant leads to a reparameterization of the family. Adding a common real constant to θ˙l,0\dot{\theta}_{l,0} and subtracting the same constant from θ˙l,\dot{\theta}_{l,\infty} leads to horizontal rotations of the surface.

In the following, we write

q=(ql,k)1lL1knlandθ˙=(θ˙h)h𝖧.q=(q_{l,k})_{\begin{subarray}{c}1\leqslant l\leqslant L\\ 1\leqslant k\leqslant n_{l}\end{subarray}}\quad\text{and}\quad\dot{\theta}=(\dot{\theta}_{h})_{h\in\mathsf{H}}.

Then a configuration refers to the pair (q,θ˙)(q,\dot{\theta}).

1.2. Force

Given a configuration (q,θ˙)(q,\dot{\theta}), let clc_{l} be the real numbers that solve

(1) nlcl+nl1cl1+θ˙l,0+θ˙l,=0,1lL+1.-n_{l}c_{l}+n_{l-1}c_{l-1}+\dot{\theta}_{l,0}+\dot{\theta}_{l,\infty}=0,\quad 1\leq l\leq L+1.

Recall the convention nl=0n_{l}=0 if l<1l<1 or l>Ll>L, so we also adopt the convention cl=0c_{l}=0 if l<1l<1 or l>Ll>L. A summation over ll yields

(2) Θ1=h𝖧θ˙h=0.\Theta_{1}=\sum_{h\in\mathsf{H}}\dot{\theta}_{h}=0.

If (2) is satisfied, the real numbers clc_{l} are determined by (1) as functions of θ˙\dot{\theta}.

For 1lL+11\leq l\leq L+1, let ψl\psi_{l} be the meromorphic 11-form on the Riemann sphere ^\hat{\mathbb{C}} with simple poles at ql,kq_{l,k} with residue cl-c_{l} for each 1knl1\leq k\leq n_{l}, at ql1,kq_{l-1,k} with residue cl1c_{l-1} for each 1knl11\leq k\leq n_{l-1}, at 0 with residue θ˙l,0\dot{\theta}_{l,0}, and at \infty with residue θ˙l,\dot{\theta}_{l,\infty}. More explicitly,

ψl=(k=1nlclzql,k+k=1nl1cl1zql1,k+θ˙l,0z)dz.\psi_{l}=\Big{(}\sum_{k=1}^{n_{l}}\frac{-c_{l}}{z-q_{l,k}}+\sum_{k=1}^{n_{l-1}}\frac{c_{l-1}}{z-q_{l-1,k}}+\frac{\dot{\theta}_{l,0}}{z}\Big{)}dz.

We then see that Equations (1) arise from the Residue Theorem

Remark 2.

In the definition of configuration, we may replace θ˙\dot{\theta} by the parameters (cl,θ˙l+1,0θ˙l,0)1lL(c_{l},\dot{\theta}_{l+1,0}-\dot{\theta}_{l,0})_{1\leq l\leq L}. Then θ˙l,0\dot{\theta}_{l,0}’s are defined up to an additive constant (corresponding to a rotation), θ˙l,\dot{\theta}_{l,\infty}’s are determined by (1), and (2) is automatically satisfied. To quotient out reparameterizations of the family, we may assume that cl=1c_{l}=1 for some 1lL1\leq l\leq L.

We define the force Fl,kF_{l,k} by

(3) Fl,k=Res(ψl2+ψl+122zdz,ql,k).F_{l,k}=\operatorname{Res}\left(\frac{\psi_{l}^{2}+\psi_{l+1}^{2}}{2}\frac{z}{dz},q_{l,k}\right).

Or, more explicitly,

(4) Fl,k=1kjnl2cl2ql,kql,kql,j1jnl+1clcl+1ql,kql,kql+1,j1jnl1clcl1ql,kql,kql1,j+cl2+cl(θ˙l+1,0θ˙l,0).F_{l,k}=\sum_{1\leq k\neq j\leq n_{l}}\frac{2c_{l}^{2}q_{l,k}}{q_{l,k}-q_{l,j}}-\sum_{1\leq j\leq n_{l+1}}\frac{c_{l}c_{l+1}q_{l,k}}{q_{l,k}-q_{l+1,j}}-\sum_{1\leq j\leq n_{l-1}}\frac{c_{l}c_{l-1}q_{l,k}}{q_{l,k}-q_{l-1,j}}\\ +c_{l}^{2}+c_{l}(\dot{\theta}_{l+1,0}-\dot{\theta}_{l,0}).

In [Li12], the force had different formula depending on the parity of ll. One verifies that both are equivalent to (4).

Remark 3 (Electrostatic interpretation).

The force equation (4) can be expressed as

Fl,k=1kjnlcl2(ql,k+ql,j)ql,kql,j1jnl+1clcl+1(ql,k+ql+1,j)2(ql,kql+1,j)1jnl1clcl1(ql,k+ql1,j)2(ql,kql1,j)+cl2(θ˙l,θ˙l,0θ˙l+1,+θ˙l+1,0).F_{l,k}=\sum_{1\leq k\neq j\leq n_{l}}\frac{c_{l}^{2}(q_{l,k}+q_{l,j})}{q_{l,k}-q_{l,j}}-\sum_{1\leq j\leq n_{l+1}}\frac{c_{l}c_{l+1}(q_{l,k}+q_{l+1,j})}{2(q_{l,k}-q_{l+1,j})}\\ -\sum_{1\leq j\leq n_{l-1}}\frac{c_{l}c_{l-1}(q_{l,k}+q_{l-1,j})}{2(q_{l,k}-q_{l-1,j})}+\frac{c_{l}}{2}(\dot{\theta}_{l,\infty}-\dot{\theta}_{l,0}-\dot{\theta}_{l+1,\infty}+\dot{\theta}_{l+1,0}).

Note that

a+bab=cothlnalnb2=2lnalnb+m=1(2lnalnb2mπi+2lnalnb+2mπi).\frac{a+b}{a-b}=\coth\frac{\ln a-\ln b}{2}=\frac{2}{\ln a-\ln b}+\sum_{m=1}^{\infty}\Big{(}\frac{2}{\ln a-\ln b-2m\pi{\rm i}}+\frac{2}{\ln a-\ln b+2m\pi{\rm i}}\Big{)}.

Disregarding absolute convergence, we write this formally as

a+bab=m2lnalnb2mπi.\frac{a+b}{a-b}=\sum_{m\in\mathbb{Z}}\frac{2}{\ln a-\ln b-2m\pi{\rm i}}.

Then the force is given, formally, by

Fl,k=0m2cl22mπi+m1kjnl2cl2lnql,klnql,j2mπim1jnl+1clcl+1lnql,klnql+1.j2mπim1jnl1clcl1lnql,klnql1.j2mπi+cl2(θ˙l,θ˙l,0θ˙l+1,+θ˙l+1,0).F_{l,k}=\sum_{0\neq m\in\mathbb{Z}}\frac{2c_{l}^{2}}{2m\pi{\rm i}}+\sum_{\begin{subarray}{c}m\in\mathbb{Z}\\ 1\leq k\neq j\leq n_{l}\end{subarray}}\frac{2c_{l}^{2}}{\ln q_{l,k}-\ln q_{l,j}-2m\pi{\rm i}}\\ -\sum_{\begin{subarray}{c}m\in\mathbb{Z}\\ 1\leq j\leq n_{l+1}\end{subarray}}\frac{c_{l}c_{l+1}}{\ln q_{l,k}-\ln q_{l+1.j}-2m\pi{\rm i}}-\sum_{\begin{subarray}{c}m\in\mathbb{Z}\\ 1\leq j\leq n_{l-1}\end{subarray}}\frac{c_{l}c_{l-1}}{\ln q_{l,k}-\ln q_{l-1.j}-2m\pi{\rm i}}\\ +\frac{c_{l}}{2}(\dot{\theta}_{l,\infty}-\dot{\theta}_{l,0}-\dot{\theta}_{l+1,\infty}+\dot{\theta}_{l+1,0}).

Recall that lnql,k+2mπi\ln q_{l,k}+2m\pi{\rm i} are the real positions of the necks. So this formal expression has an electrostatic interpretation similar to those in [Tra02b] and [Tra08]. Here, each neck interacts not only with all other necks in the same or adjacent layers, but also with background constant fields given by θ˙\dot{\theta}.

Remark 4 (Another electrostatic interpretation).

In fact, (4)/ql,k\eqref{eq:force}/q_{l,k} has a similar electrostatic interpretation. But this time, the necks are seen as placed at ql,kq_{l,k}. Each neck interacts with all other necks in the same and adjacent layers, as well as a virtual neck at 0 with “charge” cl+θ˙l+1,0θ˙l,0c_{l}+\dot{\theta}_{l+1,0}-\dot{\theta}_{l,0}. This is no surprise, as electrostatic laws are known to be preserved under conformal mappings (such as ln(z)\ln(z)).

1.3. Main result

In the following, we write F=(Fl,k)1lL,1knlF=(F_{l,k})_{1\leq l\leq L,1\leq k\leq n_{l}}.

Definition 1.

The configuration is balanced if F=0F=0 and Θ1=0\Theta_{1}=0.

Summing up all forces yields a necessary condition for the configuration to be balanced, namely

Θ2=1lL1knlFl,k=1lL+112(Res(zψl2dz,0)+Res(zψl2dz,))=1lL+1θ˙l,2θ˙l,022=0.\Theta_{2}=\sum_{\begin{subarray}{c}1\leq l\leq L\\ 1\leq k\leq n_{l}\end{subarray}}F_{l,k}=\sum_{1\leq l\leq L+1}-\frac{1}{2}\Bigg{(}\operatorname{Res}\left(\frac{z\psi_{l}^{2}}{dz},0\right)+\operatorname{Res}\left(\frac{z\psi_{l}^{2}}{dz},\infty\right)\Bigg{)}\\ =\sum_{1\leq l\leq L+1}\frac{{\dot{\theta}_{l,\infty}^{2}-\dot{\theta}_{l,0}^{2}}}{2}=0.
Lemma 1.

The Jacobian matrix (Θ1,Θ2)/θ˙\partial(\Theta_{1},\Theta_{2})/\partial\dot{\theta} has real rank 22 as long as cl0c_{l}\neq 0 for some 1lL1\leq l\leq L.

The assumption of the lemma simply says that the surface does not remain a degenerate plane to the first order.

Proof.

The proposition says that the matrix has an invertible minor of size 2×22\times 2. Explicitly, we have

(Θ1,Θ2)(θ˙l,0,θ˙l,)=(11θ˙l,0θ˙l,).\frac{\partial(\Theta_{1},\Theta_{2})}{\partial(\dot{\theta}_{l,0},\dot{\theta}_{l,\infty})}=\begin{pmatrix}1&1\\ -\dot{\theta}_{l,0}&\dot{\theta}_{l,\infty}\end{pmatrix}.

This minor is invertible if and only if the ends θ˙l,0+θ˙l,0\dot{\theta}_{l,0}+\dot{\theta}_{l,\infty}\neq 0. This must be the case for at least one 1lL1\leq l\leq L because, otherwise, we have cl=0c_{l}=0 for all 1lL1\leq l\leq L. ∎

Definition 2.

The configuration is rigid if the complex rank of F/q\partial F/\partial q is N1N-1.

Remark 5.

In fact, the complex rank of F/q\partial F/\partial q is at most N1N-1. We have seen that a complex scaling of qq corresponds to a translation of lnql,k+2mπi\ln q_{l,k}+2m\pi{\rm i}, mm\in\mathbb{Z}, which does not change the force. It then makes sense to normalize qq by fixing q1,1=1q_{1,1}=1.

Theorem 1.

Let (q,θ˙)(q,\dot{\theta}) be a balanced and rigid configuration such that cl0c_{l}\neq 0 for 1lL1\leq l\leq L. Then for τ>0\tau>0 sufficiently small, there exists a smooth family MτM_{\tau} of complete singly periodic minimal surface of genus g=NLg=N-L, period (0,0,2π)(0,0,2\pi), and 2(L+1)2(L+1) Scherk ends such that, as τ0\tau\to 0,

  • MτM_{\tau} converges to an (L+1)(L+1)-sheeted xzxz-plane with singular points at lnql,k+2mπi\ln q_{l,k}+2m\pi{\rm i}, mm\in\mathbb{Z}. Here, the xzxz-plane is identified to the complex plane \mathbb{C}, with xx-axis (resp. zz-axis) identified to the real (resp. imaginary) axis.

  • After suitable scaling and translation, each singular point opens up into a neck that converges to a catenoid.

  • The unit vector in the direction of each Scherk end hh has the yy-component τθ˙h+𝒪(τ2)\tau\dot{\theta}_{h}+\mathcal{O}(\tau^{2}).

Moreover, MτM_{\tau} is embedded if

(5) θ˙1,0>>θ˙L+1,0andθ˙1,>>θ˙L+1,.\dot{\theta}_{1,0}>\cdots>\dot{\theta}_{L+1,0}\quad\text{and}\quad\dot{\theta}_{1,\infty}>\cdots>\dot{\theta}_{L+1,\infty}.
Remark 6.

MτM_{\tau} also depends smoothly on θ˙\dot{\theta} belonging to the local smooth manifold defined by Θ1=0\Theta_{1}=0 and Θ2=0\Theta_{2}=0. Up to reparameterizations of the family and horizontal rotations, we obtain families parameterized by 2L12L-1 parameters. Since we have 2(L+1)2(L+1) Scherk ends, this parameter count is compatible with the fact that Karcher–Scherk saddle towers with 2k2k ends form a family parameterized by 2k32k-3 parameters.

Remark 7.

If the embeddedness condition (5) is satisfied and Θ1=0\Theta_{1}=0, the sequence θ˙l,0+θ˙l,\dot{\theta}_{l,0}+\dot{\theta}_{l,\infty} is strictly monotonically decreasing, and changes sign once and only once. Then the sequence nlcln_{l}c_{l} is strictly concave (i.e. nl1cl1+nl+1cl+1<2nlcln_{l-1}c_{l-1}+n_{l+1}c_{l+1}<2n_{l}c_{l} for 1lL1\leq l\leq L). Hence clc_{l}, 1lL1\leq l\leq L, are strictly positive, and the condition of Lemma 1 is satisfied.

Remark 8.

We could allow some clc_{l} to be negative, with the price of losing embeddedness. Even worse, with negative clc_{l}, the vertical planes in the limit will not be geometrically ordered as they are labeled. For instance, if L=2,c1>0L=2,c_{1}>0, but c2<0c_{2}<0, then the catenoid necks, as well as the 1st and 3rd “planes”, will all lie on the same side of the 2nd “plane”.

Remark 9.

We did not allow any clc_{l} to be 0 in Theorem 1. Otherwise, the surface might still have nodes. In that case, the claimed family might not be smooth, and the claimed genus would be incorrect.

2. Examples

2.1. Surfaces of genus 0

When the genus g=NL=0g=N-L=0, we have nl=1n_{l}=1 for all 1lL1\leq l\leq L, i.e. there is only one neck on every layer. It then makes sense to drop the subscript kk. For instance, the position and the force for the neck on layer ll are simply denoted by qlq_{l} and FlF_{l}. We assume L>1L>1 in this part.

In this case, if Θ1=0\Theta_{1}=0, Equation (1) can be explicitly solved by

cl=i=1l(θ˙i,0+θ˙i,),1lL,c_{l}=\sum_{i=1}^{l}(\dot{\theta}_{i,0}+\dot{\theta}_{i,\infty}),\quad 1\leq l\leq L,

and the force can be written in the form

Fl=Q~l+Q~l1+cl(θ˙l,+θ˙l+1,0),1lL,F_{l}=-\widetilde{Q}_{l}+\widetilde{Q}_{l-1}+c_{l}(\dot{\theta}_{l,\infty}+\dot{\theta}_{l+1,0}),\quad 1\leq l\leq L,

where we changed to the parameters

Q~l=cl+1cl1ql+1/ql,1l<L,\widetilde{Q}_{l}=\frac{c_{l+1}c_{l}}{1-q_{l+1}/q_{l}},\quad 1\leq l<L,

with the convention that Q~0=Q~L=0\widetilde{Q}_{0}=\widetilde{Q}_{L}=0. Then the forces are linear in Q~\widetilde{Q} and, if Θ2=0\Theta_{2}=0, the balance condition F=0F=0 is uniquely solved by

(6) Q~l=i=1lci(θ˙i+1,0+θ˙i,)=i=l+1Lci(θ˙i+1,0+θ˙i,),1l<L.\widetilde{Q}_{l}=\sum_{i=1}^{l}c_{i}(\dot{\theta}_{i+1,0}+\dot{\theta}_{i,\infty})=-\sum_{i=l+1}^{L}c_{i}(\dot{\theta}_{i+1,0}+\dot{\theta}_{i,\infty}),\quad 1\leq l<L.

Therefore, if we fix q1=1q_{1}=1, all other qlq_{l}, 1<lL1<l\leq L are uniquely determined.

Recall from Remark 7 that, under the embeddedness condition (5), the numbers clc_{l}, 1lL1\leq l\leq L, are positive. Moreover, the summands in (6) changes sign at most once, so the sequence Q~\widetilde{Q} is unimodal, i.e. there exists 1l<L1\leq l^{\prime}<L such that

0=Q~0Q~1Q~lQ~L1Q~L=0.0=\widetilde{Q}_{0}\leq\widetilde{Q}_{1}\leq\cdots\leq\widetilde{Q}_{l^{\prime}}\geq\cdots\geq\widetilde{Q}_{L-1}\geq\widetilde{Q}_{L}=0.

Hence Q~l\widetilde{Q}_{l}, 1lL1\leq l\leq L, are non-negative. Moreover,

Q~l<i=1lci(θ˙i,0+θ˙i,)\displaystyle\widetilde{Q}_{l}<\sum_{i=1}^{l}c_{i}(\dot{\theta}_{i,0}+\dot{\theta}_{i,\infty}) =i=1l(ci2ci1ci)cl2cl+1cl\displaystyle=\sum_{i=1}^{l}(c_{i}^{2}-c_{i-1}c_{i})\leq c_{l}^{2}\leq c_{l+1}c_{l} if l<l,\displaystyle\text{if }l<l^{\prime},
Q~l<i=l+1Lci(θ˙i+1,0+θ˙i+1,)\displaystyle\widetilde{Q}_{l}<-\sum_{i=l+1}^{L}c_{i}(\dot{\theta}_{i+1,0}+\dot{\theta}_{i+1,\infty}) =i=l+1L(ci2ci+1ci)cl+12cl+1cl\displaystyle=\sum_{i=l+1}^{L}(c_{i}^{2}-c_{i+1}c_{i})\leq c_{l+1}^{2}\leq c_{l+1}c_{l} if ll.\displaystyle\text{if }l\geq l^{\prime}.

So qq consists of real numbers and ql+1/ql<0q_{l+1}/q_{l}<0 for all 1l<L1\leq l<L.

We have proved that

Proposition 2.

If the genus g=NL=0g=N-L=0, and θ˙\dot{\theta} satisfies the balancing condition Θ1=Θ2=0\Theta_{1}=\Theta_{2}=0 as well as the embeddedness condition (5), then up to complex scalings, there exist unique values for the parameters qq, depending analytically on θ˙\dot{\theta}, such that the configuration (q,θ˙)(q,\dot{\theta}) is balanced. Moreover, all such configurations are rigid. If we fix q1=1q_{1}=1, then qq consist of real numbers, and we have ql>0q_{l}>0 (resp. <0<0) if ll is odd (resp. even).

2.2. Surfaces with four ends

When L=1L=1, Θ1=Θ2=0\Theta_{1}=\Theta_{2}=0 implies that

θ˙1,0+θ˙2,=θ˙2,0+θ˙1,=0.\dot{\theta}_{1,0}+\dot{\theta}_{2,\infty}=\dot{\theta}_{2,0}+\dot{\theta}_{1,\infty}=0.

Up to reparameterizations of the family, we may assume that c1=1c_{1}=1. It makes sense to drop the subscript ll in other notations, and write FkF_{k} for F1,kF_{1,k}, qkq_{k} for q1,kq_{1,k}, and nn for n1n_{1}. The goal of this part is to prove the following classification result.

Proposition 3.

Up to a complex scaling, a configuration with L=1L=1 and nn nodes must be given by qk=exp(2πik/n)q_{k}=\exp(2\pi{\rm i}k/n), and such a configuration is rigid.

Such a configuration is an nn-covering of the configuration for Scherk saddle towers. As a consequence, the arising minimal surfaces are nn-coverings of Scherk saddle towers. This is compatible with the result of [MW07] that the Scherk saddle towers are the only connected SPMSs with four Scherk ends.

Proof.

To find the positions qkq_{k} such that

(7) Fk=1kjn2qkqkqj(n1)=0,1kn,F_{k}=\sum_{1\leq k\neq j\leq n}\frac{2q_{k}}{q_{k}-q_{j}}-(n-1)=0,\qquad 1\leq k\leq n,

we use the polynomial method: Consider the polynomial

P(z)=k=1n(zqk).P(z)=\prod_{k=1}^{n}(z-q_{k}).

Then we have

P\displaystyle P^{\prime} =Pk=1n1zqk\displaystyle=P\sum_{k=1}^{n}\frac{1}{z-q_{k}}
P′′\displaystyle P^{\prime\prime} =Pk=1n1kjn1zqj1zqk=2Pk=1n1zqk1kjn1qkqj\displaystyle=P\sum_{k=1}^{n}\sum_{1\leq k\neq j\leq n}\frac{1}{z-q_{j}}\frac{1}{z-q_{k}}=2P\sum_{k=1}^{n}\frac{1}{z-q_{k}}\sum_{1\leq k\neq j\leq n}\frac{1}{q_{k}-q_{j}}
=Pk=1nn1qk(zqk)=(n1)Pk=1n1z(1qk+1zqk)by (7)\displaystyle=P\sum_{k=1}^{n}\frac{n-1}{q_{k}(z-q_{k})}=(n-1)P\sum_{k=1}^{n}\frac{1}{z}\Big{(}\frac{1}{q_{k}}+\frac{1}{z-q_{k}}\Big{)}\qquad\text{by~{}\eqref{eq:balance4ends}}
=n1z(PP(0)P(0)P)\displaystyle=\frac{n-1}{z}\Big{(}P^{\prime}-\frac{P^{\prime}(0)}{P(0)}P\Big{)}

For the last equation to have a polynomial solution, we must have P(0)=0P^{\prime}(0)=0. Otherwise, the left-hand side would be a polynomial of degree n2n-2, but the right-hand side would be a polynomial of degree n1n-1.

Consequently, Fk=0F_{k}=0 if and only if

zP′′(z)(n1)P(z)=0,zP^{\prime\prime}(z)-(n-1)P^{\prime}(z)=0,

which, up to a complex scaling, is uniquely solved by

P(z)=zn1.P(z)=z^{n}-1.

So a balanced 4-end configuration must be given by the roots of unity qk=exp(2πik/n)q_{k}=\exp(2\pi{\rm i}k/n), 0kn10\leq k\leq n-1.

We now verify that the configuration is rigid. For this purpose, we compute

Fkqj={2qk(qkqj)2,jk;21kinqi(qkqi)2,j=k.\frac{\partial F_{k}}{\partial q_{j}}=\begin{dcases}2\frac{q_{k}}{(q_{k}-q_{j})^{2}},&j\neq k;\\ 2\sum_{1\leq k\neq i\leq n}\frac{-q_{i}}{(q_{k}-q_{i})^{2}},&j=k.\end{dcases}

Note that j=1nqjFk/qj=0\sum_{j=1}^{n}q_{j}\partial F_{k}/\partial q_{j}=0 while

qjFkqj=2qjqk(qkqj)2=2e2πij+kn(e2πijne2πikn)2<0q_{j}\frac{\partial F_{k}}{\partial q_{j}}=2\frac{q_{j}q_{k}}{(q_{k}-q_{j})^{2}}=2\frac{e^{2\pi{\rm i}\frac{j+k}{n}}}{(e^{2\pi{\rm i}\frac{j}{n}}-e^{2\pi{\rm i}\frac{k}{n}})^{2}}\in\mathbb{R}_{<0}

when jkj\neq k, so the matrix

Fqdiag(q1,,qn)\frac{\partial F}{\partial q}\operatorname{diag}(q_{1},\cdots,q_{n})

has real entries, has a kernel of complex dimension 11 (spanned by the all-one vector), and any of its principal submatrix is diagonally dominant. We then conclude that the matrix, as well as the Jacobian F/q\partial F/\partial q, has a complex rank n1n-1. This finishes the proof of rigidity. ∎

Remark 10.

The perturbation argument as in the proof of [Tra02b, Proposition 1] also applies here, word by word, to prove the rigidity.

2.3. Gluing two saddle towers of different periods

We want to construct a smooth family of configurations depending on a positive real number λ\lambda such that, for small λ\lambda, the configuration looks like two columns of nodes far away from each other, one with period 2π/n12\pi/n_{1}, and the other with period 2π/n22\pi/n_{2}. If balanced and rigid, these configurations would give rise to minimal surfaces that look like two Scherk saddle towers with different periods that are glued along a pair of ends. The construction is in the same spirit as [Tra02b, § 2.5] and [Tra08, § 4.3.4].

Proposition 4.

For a real number λ>0\lambda>0 sufficiently small, there are balanced and rigid configurations (q(λ),θ˙(λ))(q(\lambda),\dot{\theta}(\lambda)) with L=2L=2 depending smoothly on λ\lambda such that, at λ=0\lambda=0,

q2,jq1,k=0,1kn1,1jn2.\frac{q_{2,j}}{q_{1,k}}=0,\qquad 1\leq k\leq n_{1},1\leq j\leq n_{2}.

Up to a complex scaling and reparameterization, we may fix q1,1=1q_{1,1}=1, and write q2,1=λexp(iϕ)q_{2,1}=\lambda\exp({\rm i}\phi). Then, at λ=0\lambda=0, we have

(8) θ˙1,0+θ˙2,=θ˙2,0+θ˙3,=θ˙3,0+θ˙1,=0\dot{\theta}_{1,0}+\dot{\theta}_{2,\infty}=\dot{\theta}_{2,0}+\dot{\theta}_{3,\infty}=\dot{\theta}_{3,0}+\dot{\theta}_{1,\infty}=0

and,

q1,k\displaystyle q_{1,k} =exp(k1n12πi),\displaystyle=\exp\Big{(}\frac{k-1}{n_{1}}2\pi{\rm i}\Big{)}, 1kn1,\displaystyle 1\leq k\leq n_{1},
q~2,k:=q2,k/q2,1\displaystyle\widetilde{q}_{2,k}:=q_{2,k}/q_{2,1} =exp(k1n22πi),\displaystyle=\exp\Big{(}\frac{k-1}{n_{2}}2\pi{\rm i}\Big{)}, 1kn2,\displaystyle 1\leq k\leq n_{2},

where ϕlcm(n1,n2)\phi\operatorname{lcm}(n_{1},n_{2}) is necessarily a multiple of π\pi.

In other words, the construction only works if the configuration admits a reflection symmetry.

Remark 11.

The first named author was shown a video suggesting that, when two Scherk saddle towers are glued into a minimal surface, one can slide one saddle tower with respect to the other while the surface remains minimal. The proposition above suggests that this is not possible.

In fact, the family of configurations also depends on θ˙\dot{\theta} belonging to the local manifold defined by Θ1=Θ2=0\Theta_{1}=\Theta_{2}=0 and (one equation from) (8). Up to rotations of the configuration and reparameterizations of the family of minimal surfaces, the family of configurations is parameterized, as expected, by two parameters.

Proof.

Let us first study the situation at λ=0\lambda=0. We compute at λ=0\lambda=0

F1,kc12=\displaystyle\frac{F_{1,k}}{c_{1}^{2}}= 1kjn12q1,kq1,kq1,j1jn2c2c1q1,kq1,kq2,j+1+θ˙2,0θ˙1,0c1\displaystyle\sum_{1\leq k\neq j\leq n_{1}}\frac{2q_{1,k}}{q_{1,k}-q_{1,j}}-\sum_{1\leq j\leq n_{2}}\frac{c_{2}}{c_{1}}\frac{q_{1,k}}{q_{1,k}-q_{2,j}}+1+\frac{\dot{\theta}_{2,0}-\dot{\theta}_{1,0}}{c_{1}}
=\displaystyle= 1kjn12q1,kq1,kq1,jn2c2c1+1+θ˙2,0θ˙1,0c1,\displaystyle\sum_{1\leq k\neq j\leq n_{1}}\frac{2q_{1,k}}{q_{1,k}-q_{1,j}}-n_{2}\frac{c_{2}}{c_{1}}+1+\frac{\dot{\theta}_{2,0}-\dot{\theta}_{1,0}}{c_{1}},
F2,kc22=\displaystyle\frac{F_{2,k}}{c_{2}^{2}}= 1kjn22q2,kq2,kq2,j1jn1c1c2q2,kq2,kq1,j+1+θ˙3,0θ˙2,0c2\displaystyle\sum_{1\leq k\neq j\leq n_{2}}\frac{2q_{2,k}}{q_{2,k}-q_{2,j}}-\sum_{1\leq j\leq n_{1}}\frac{c_{1}}{c_{2}}\frac{q_{2,k}}{q_{2,k}-q_{1,j}}+1+\frac{\dot{\theta}_{3,0}-\dot{\theta}_{2,0}}{c_{2}}
=\displaystyle= 1kjn22q2,kq2,kq2,j+1+θ˙3,0θ˙2,0c2.\displaystyle\sum_{1\leq k\neq j\leq n_{2}}\frac{2q_{2,k}}{q_{2,k}-q_{2,j}}+1+\frac{\dot{\theta}_{3,0}-\dot{\theta}_{2,0}}{c_{2}}.

Write Gl=kFl,kG_{l}=\sum_{k}F_{l,k}. Summing the above over kk gives, at λ=0\lambda=0,

1n1G1c12=n1n2c2c1+θ˙2,0θ˙1,0c1,1n2G2c22=n2+θ˙3,0θ˙2,0c2.\frac{1}{n_{1}}\frac{G_{1}}{c_{1}^{2}}=n_{1}-n_{2}\frac{c_{2}}{c_{1}}+\frac{\dot{\theta}_{2,0}-\dot{\theta}_{1,0}}{c_{1}},\qquad\frac{1}{n_{2}}\frac{G_{2}}{c_{2}^{2}}=n_{2}+\frac{\dot{\theta}_{3,0}-\dot{\theta}_{2,0}}{c_{2}}.

So G1=G2=0G_{1}=G_{2}=0 at λ=0\lambda=0 only if

0=\displaystyle 0= (θ˙2,0+θ˙3,)=θ˙3,0θ˙2,0+n2c2\displaystyle-(\dot{\theta}_{2,0}+\dot{\theta}_{3,\infty})=\dot{\theta}_{3,0}-\dot{\theta}_{2,0}+n_{2}c_{2}
=\displaystyle= (θ˙1,0+θ˙2,)=n1c1n2c2+θ˙2,0θ˙1,0.\displaystyle-(\dot{\theta}_{1,0}+\dot{\theta}_{2,\infty})=n_{1}c_{1}-n_{2}c_{2}+\dot{\theta}_{2,0}-\dot{\theta}_{1,0}.

This together with Θ1=0\Theta_{1}=0 proves (8).

Now assume that (8) is satisfied. Then we have, at λ=0\lambda=0

F1,kc12=\displaystyle\frac{F_{1,k}}{c_{1}^{2}}= 1kjn12q1,kq1,kq1,j(n11),\displaystyle\sum_{1\leq k\neq j\leq n_{1}}\frac{2q_{1,k}}{q_{1,k}-q_{1,j}}-(n_{1}-1),
F2,kc22=\displaystyle\frac{F_{2,k}}{c_{2}^{2}}= 1kjn22q2,kq2,kq2,j(n21).\displaystyle\sum_{1\leq k\neq j\leq n_{2}}\frac{2q_{2,k}}{q_{2,k}-q_{2,j}}-(n_{2}-1).

These expressions are identical to the force (7) for single layer configurations. So we know for l=1,2l=1,2 that, at λ=0\lambda=0, the configuration is balanced only if

q~l,k:=ql,kql,1=exp(k1nl2πi).\widetilde{q}_{l,k}:=\frac{q_{l,k}}{q_{l,1}}=\exp\Big{(}\frac{k-1}{n_{l}}2\pi{\rm i}\Big{)}.

Up to complex scaling, we may fix q1,1=1q_{1,1}=1 so q~1,k=q1,k\widetilde{q}_{1,k}=q_{1,k}. And up to reparameterization of the family (of configurations), we write q2,1=λexp(iϕ)q_{2,1}=\lambda\exp({\rm i}\phi).

Now assume these initial values for q~l,k\widetilde{q}_{l,k}. Then we have, at λ=0\lambda=0,

G2c1c2=\displaystyle\frac{G_{2}}{c_{1}c_{2}}= k=1n2j=1n1q2,kq2,kq1,j=k=1n2j=1n1m=1(q2,kq1,j)m\displaystyle-\sum_{k=1}^{n_{2}}\sum_{j=1}^{n_{1}}\frac{q_{2,k}}{q_{2,k}-q_{1,j}}=\sum_{k=1}^{n_{2}}\sum_{j=1}^{n_{1}}\sum_{m=1}^{\infty}\Big{(}\frac{q_{2,k}}{q_{1,j}}\Big{)}^{m}
=\displaystyle= k=1n2j=1n1m=1q2,1mexp(2miπ(k1n2j1n1))\displaystyle\sum_{k=1}^{n_{2}}\sum_{j=1}^{n_{1}}\sum_{m=1}^{\infty}q_{2,1}^{m}\exp\bigg{(}2m{\rm i}\pi\Big{(}\frac{k-1}{n_{2}}-\frac{j-1}{n_{1}}\Big{)}\bigg{)}

Seen as a power series of q2,1q_{2,1}, the coefficient for q2,1mq_{2,1}^{m} is

k=1n2j=1n1exp(2miπ(k1n2j1n1)).\sum_{k=1}^{n_{2}}\sum_{j=1}^{n_{1}}\exp\bigg{(}2m{\rm i}\pi\Big{(}\frac{k-1}{n_{2}}-\frac{j-1}{n_{1}}\Big{)}\bigg{)}.

It is non-zero only if mm is a common multiple of n1n_{1} and n2n_{2}, in which case the coefficient of q2,1mq_{2,1}^{m} equals n1n2n_{1}n_{2}. In particular, let μ=lcm(n1,n2)\mu=\operatorname{lcm}(n_{1},n_{2}), then at λ=0\lambda=0,

(9) ImG2λμ=c1c2n1n2sin(μϕ)\operatorname{Im}\frac{G_{2}}{\lambda^{\mu}}=c_{1}c_{2}n_{1}n_{2}\sin(\mu\phi)

vanishes if and only if μϕ\mu\phi is a multiple of π\pi.

Now we use the Implicit Function Theorem to find balance configurations with λ>0\lambda>0. From the proof for Proposition 3, we know that (Fl,kq~l,j)2j,knl\big{(}\frac{\partial F_{l,k}}{\partial\widetilde{q}_{l,j}}\big{)}_{2\leq j,k\leq n_{l}}, l=1,2l=1,2, are invertible. Hence for λ\lambda sufficiently small, there exist unique values for (q~l,k)l=1,2;2knl(\widetilde{q}_{l,k})_{l=1,2;2\leq k\leq n_{l}}, depending smoothly on λ\lambda, θ˙\dot{\theta}, and ϕ\phi, such that (Fl,k)l=1,2;2knl=0(F_{l,k})_{l=1,2;2\leq k\leq n_{l}}=0. By (9), there exists a unique value for ϕ\phi, depending smoothly on λ\lambda and θ˙\dot{\theta}, such that ImG2/λμ=0\operatorname{Im}G_{2}/\lambda^{\mu}=0. Note also that ReG2\operatorname{Re}G_{2} is linear in θ˙\dot{\theta}. By Lemma 1, the solutions (λ,θ˙)(\lambda,\dot{\theta}) to ReG2=0\operatorname{Re}G_{2}=0 and Θ1=Θ2=0\Theta_{1}=\Theta_{2}=0 form a manifold of dimension 44 (including multiplication by common real factor on θ˙\dot{\theta} and rotation of the configuration). Finally, we have G1=0G_{1}=0 by the Residue Theorem, and the balance is proved.

For the rigidity of the configurations with sufficiently small λ\lambda, we need to prove that the matrix

((F1,kq1,j)2j,kn1(F2,kq~2,j)2j,kn2G2q2,1)\begin{pmatrix}\big{(}\frac{\partial F_{1,k}}{\partial q_{1,j}}\big{)}_{2\leq j,k\leq n_{1}}&&\\ &\big{(}\frac{\partial F_{2,k}}{\partial\widetilde{q}_{2,j}}\big{)}_{2\leq j,k\leq n_{2}}&\\ &&\frac{\partial G_{2}}{\partial q_{2,1}}\end{pmatrix}

is invertible. We know that the first two blocks are invertible at λ=0\lambda=0. By continuity, they remain invertible for λ\lambda sufficiently small. The last block is clearly non-zero for λ0\lambda\neq 0 sufficiently small. ∎

2.4. Surfaces with six ends of type (n,1)

In this section, we investigate examples with L=2L=2 (hence six ends), n1=nn_{1}=n, n2=1n_{2}=1. Up to a reparameterization of the family, we may assume that c1=1c_{1}=1. Up to a complex scaling, we may assume that q2,1=1q_{2,1}=1.

We will prove that q1,kq_{1,k}’s are given by the roots of hypergeometric polynomials. Let us first recall their definitions. A hypergeometric function is defined by

F12(a,b;c;z)=k=0(a)k(b)k(c)kzkk!{{}_{2}F_{1}}(a,b;c;z)=\sum_{k=0}^{\infty}\frac{(a)_{k}(b)_{k}}{(c)_{k}}\frac{z^{k}}{k!}

with a,b,ca,b,c\in\mathbb{C}, cc is not a non-positive integer,

(a)k=a(a+1)(a+k1)=Γ(a+k)Γ(a),(a)_{k}=a(a+1)\cdots(a+k-1)=\frac{\Gamma(a+k)}{\Gamma(a)},

and (a)0=1(a)_{0}=1. The hypergeometric function w=F12(a,b;c;z)w={{}_{2}F_{1}}(a,b;c;z) solves the hypergeometric differential equation

(10) z(1z)w′′+[c(a+b+1)z]wabw=0.z(1-z)w^{\prime\prime}+[c-(a+b+1)z]w^{\prime}-abw=0.

If a=na=-n is a negative integer,

F12(n,b;c;z):=k=0n(1)k(nk)(b)k(c)kzk{{}_{2}F_{1}}(-n,b;c;z):=\sum_{k=0}^{n}(-1)^{k}\binom{n}{k}\frac{(b)_{k}}{(c)_{k}}z^{k}

is a polynomial of degree nn, and is referred to as a hypergeometric polynomial.

Proposition 5.

Let (q,θ˙)(q,\dot{\theta}) be a balanced configuration with L=2L=2, c1=1c_{1}=1, n1=nn_{1}=n, n2=1n_{2}=1. Then, up to a complex scaling, we have q2,1=1q_{2,1}=1 and (q1,k)1kn(q_{1,k})_{1\leq k\leq n} are the roots of the hypergeometric polynomial F12(n,b;c;z){{}_{2}F_{1}}(-n,b;c;z) with

b:=nc2+θ˙2,0θ˙1,0,c:=1+θ˙2,0θ˙1,0.b:=n-c_{2}+\dot{\theta}_{2,0}-\dot{\theta}_{1,0},\qquad c:=1+\dot{\theta}_{2,0}-\dot{\theta}_{1,0}.

Moreover, as long as bb and cc are not non-positive integers, and cbc-b is not a non-positive integer bigger than n-n, the configuration is rigid.

Proof.

The force equations are

F1,k=1kjn2q1,kq1,kq1,jq1,kc2q1,k1+c,1kn,F2,1=j=1nc21q1,j+c22+c2(θ˙3,0θ˙2,0),\begin{split}F_{1,k}&=\sum_{1\leq k\neq j\leq n}\frac{2q_{1,k}}{q_{1,k}-q_{1,j}}-\frac{q_{1,k}c_{2}}{q_{1,k}-1}+c,1\leq k\leq n,\\ F_{2,1}&=-\sum_{j=1}^{n}\frac{c_{2}}{1-q_{1,j}}+c_{2}^{2}+c_{2}(\dot{\theta}_{3,0}-\dot{\theta}_{2,0}),\end{split}

where c:=1+θ˙2,0θ˙1,0c:=1+\dot{\theta}_{2,0}-\dot{\theta}_{1,0}. To solve F1,k=0F_{1,k}=0 for k=1,2,,nk=1,2,\ldots,n, we use again the polynomial method: Let P(z)=k=1n(zq1,k)P(z)=\prod_{k=1}^{n}(z-q_{1,k}). Then we have

P\displaystyle P^{\prime} =Pk=1n1zq1,k;\displaystyle=P\sum_{k=1}^{n}\frac{1}{z-q_{1,k}};
P′′\displaystyle P^{\prime\prime} =2Pk=1n1zq1,k1kjn1q1,kq1,j\displaystyle=2P\sum_{k=1}^{n}\frac{1}{z-q_{1,k}}\sum_{1\leq k\neq j\leq n}\frac{1}{q_{1,k}-q_{1,j}}
=Pk=1n1(zq1,k)(c2q1,k1cq1,k)by F1,k=0\displaystyle=P\sum_{k=1}^{n}\frac{1}{(z-q_{1,k})}\Big{(}\frac{c_{2}}{q_{1,k}-1}-\frac{c}{q_{1,k}}\Big{)}\qquad\text{by $F_{1,k}=0$}
=Pk=1n(c2(z1)(zq1,k)+c2(z1)(q1,k1)cz(zq1,k)czq1,k).\displaystyle=P\sum_{k=1}^{n}\Big{(}\frac{c_{2}}{(z-1)(z-q_{1,k})}+\frac{c_{2}}{(z-1)(q_{1,k}-1)}-\frac{c}{z(z-q_{1,k})}-\frac{c}{zq_{1,k}}\Big{)}.

So the configuration is balanced if and only if

(11) P′′+(c2z1+cz)P+(c2z1P(1)P(1)czP(0)P(0))P=0.P^{\prime\prime}+\Big{(}\frac{-c_{2}}{z-1}+\frac{c}{z}\Big{)}P^{\prime}+\Big{(}\frac{c_{2}}{z-1}\frac{P^{\prime}(1)}{P(1)}-\frac{c}{z}\frac{P^{\prime}(0)}{P(0)}\Big{)}P=0.

Define

b:=n1c2+c.b:=n-1-c_{2}+c.

For (11) to have a polynomial solution of degree nn, we must have

c2P(1)P(1)=cP(0)P(0)=nb,c_{2}\frac{P^{\prime}(1)}{P(1)}=c\frac{P^{\prime}(0)}{P(0)}=-nb,

so that the leading coefficients cancel. Then (11) becomes the hypergeometric differential equation

z(1z)P′′+[c(n+b+1)z]P+nbP=0z(1-z)P^{\prime\prime}+[c-(-n+b+1)z]P^{\prime}+nbP=0

to which the only polynomial solution (up to a multiplicative constant) is given by the hypergeometric polynomial P(z)=F12(n,b;c;z)P(z)={{}_{2}F_{1}}(-n,b;c;z) of degree nn.

Moreover, in order for F2,1=0F_{2,1}=0, we must have

(12) θ˙3,0θ˙2,0=j=1n11q1,jc2=P(1)P(1)c2=nbc2c2\dot{\theta}_{3,0}-\dot{\theta}_{2,0}=\sum_{j=1}^{n}\frac{1}{1-q_{1,j}}-c_{2}=\frac{P^{\prime}(1)}{P(1)}-c_{2}=-\frac{nb}{c_{2}}-c_{2}

Note that bb and cc are real. If bb is not a non-positive integer, and cbc-b is not a non-positive integer bigger than n-n, then all the nn roots of P(z)=F12(n,b;c;z)P(z)={{}_{2}F_{1}}(-n,b;c;z) are simple. Indeed, under these assumptions, we have P(0)=1P(0)=1 and P(1)=(cb)n/(c)n0P(1)=(c-b)_{n}/(c)_{n}\neq 0 by the Chu–Vandermonde identity. Let z0z_{0} be a root of P(z)P(z), then z00,1z_{0}\neq 0,1. In view of the hypergeometric differential equation, if z0z_{0} is not simple, we have P(z0)=P(z0)=0P(z_{0})=P^{\prime}(z_{0})=0 hence P(z)0P(z)\equiv 0 by uniqueness theorem.

The rigidity means that no perturbation of q1,kq_{1,k} preserve the balance to the first order. To prove this fact, we use a perturbation argument similar to that in the proof of [Tra02b, Proposition 1].

Let (q1,k(t))1kn(q_{1,k}(t))_{1\leq k\leq n} be a deformation of the configuration such that q1,k(0)=q1,kq_{1,k}(0)=q_{1,k} and (F˙1,k(0))1kn=0(\dot{F}_{1,k}(0))_{1\leq k\leq n}=0, where dot denotes derivative with respect to tt. Define

Pt(z)=j=0naj(t)zj:=k=1n(zq1,k(t)).P_{t}(z)=\sum_{j=0}^{n}a_{j}(t)z^{j}:=\prod_{k=1}^{n}(z-q_{1,k}(t)).

Then we have

z(1z)Pt′′+[c(n+b+1)z]Pt+nbPt=o(t),z(1-z)P_{t}^{\prime\prime}+[c-(-n+b+1)z]P_{t}^{\prime}+nbP_{t}=o(t),

meaning that the coefficients from the left side are all o(t)o(t). So the coefficients of PtP_{t} must satisfy

(13) (b+j)(nj)aj(t)+(j2+j+cj)aj+1(t)=o(t),0jn.(b+j)(n-j)a_{j}(t)+(j^{2}+j+cj)a_{j+1}(t)=o(t),\qquad 0\leq j\leq n.

Note that Pt(z)P_{t}(z) is monic by definition, meaning that an(t)1a_{n}(t)\equiv 1. Since bb and cc are not non-positive integers, we conclude that aj(t)=o(t)a_{j}(t)=o(t) for all 0jn0\leq j\leq n. The simple roots depend analytically on the coefficients, so q1,k(t)=q1,k+o(t)q_{1,k}(t)=q_{1,k}+o(t). ∎

The simple roots of F12(n,b;c;z){{}_{2}F_{1}}(-n,b;c;z) are either real or form conjugate pairs. As a consequence, if rigid, the configurations in the proposition above will give rise to minimal surfaces with horizontal symmetry planes.

Example 1.

For each integer n2n\geq 2, the real parameters (b,c)(b,c) for which F12(n,b;c;z){{}_{2}F_{1}}(-n,b;c;z) has only real simple roots has been enumerated in [DJJ13]. The results are plotted in blue in Figure 1. The embeddedness conditions (5) are

θ˙1,0>θ˙2,0\displaystyle\dot{\theta}_{1,0}>\dot{\theta}_{2,0} c<1,\displaystyle\Rightarrow c<1,
θ˙1,>θ˙2,\displaystyle\dot{\theta}_{1,\infty}>\dot{\theta}_{2,\infty} b>n,\displaystyle\Rightarrow b>-n,
θ˙2,0>θ˙3,0\displaystyle\dot{\theta}_{2,0}>\dot{\theta}_{3,0} c22>nb,\displaystyle\Rightarrow c_{2}^{2}>-nb,
θ˙2,>θ˙3,\displaystyle\dot{\theta}_{2,\infty}>\dot{\theta}_{3,\infty} c22>n(c2+b),\displaystyle\Rightarrow c_{2}^{2}>n(c_{2}+b),

where c2=n1b+cc_{2}=n-1-b+c. The region defined by these is plotted in red in Figure 1. Then non-integer parameters (b,c)(b,c) in the intersection of red and blue regions give rise to balanced and rigid configurations with real q1,kq_{1,k}.

Refer to caption
Figure 1. The set of bb and cc for which F12(n,b;c;z){{}_{2}F_{1}}(-n,b;c;z) has only real simple roots (blue), and for which the embeddedness conditions are satisfied (red).

Figure 2 shows the configurations of three examples with n=5n=5. ∎

Refer to caption
b=3.4,c=0.1b=-3.4,c=-0.1
Refer to caption
b=3.4,c=0.1b=-3.4,c=0.1
Refer to caption
b=4.001,c=0.5b=-4.001,c=0.5
Figure 2. (5,1)(5,1) balanced configurations. The circles and squares represent the necks at levels one and two respectively.
Remark 12.

As c0c\to 0, F12(n,b;c;z)/Γ(c){{}_{2}F_{1}}(-n,b;c;z)/\Gamma(c) converges to a polynomial with a root at 0. One may interpret that, as cc increases across 0, a root moves from the interval (,0)(-\infty,0) to the interval (0,1)(0,1) through 0.

When b=1nb=1-n, F12(n,b;c;z){{}_{2}F_{1}}(-n,b;c;z) becomes a polynomial of degree n1n-1. One may interprete that, as bb increases across 1n1-n, a root moves from the interval (,0)(-\infty,0) to the interval (1,)(1,\infty) through the infinity.

Example 2.

Assume that b+c=1nb+c=1-n (hence c2=2bc_{2}=-2b). Then by the identity

F12(n,b;c;z)=(b)n(c)n(z)nF12(n,1cn;1bn;1z),{{}_{2}F_{1}}(-n,b;c;z)=\frac{(b)_{n}}{(c)_{n}}(-z)^{n}{{}_{2}F_{1}}\left(-n,1-c-n;1-b-n;\frac{1}{z}\right),

the simple roots must be symmetrically placed. That is, if z0z_{0} is a root, so is 1/z01/z_{0}. This symmetry appears in the resulting minimal surfaces as a rotational symmetry. If the simple roots are real, the rotation reduces to a vertical reflectional. In view of Figure 1, we obtain the following concrete examples.

  • n2n\geq 2 and 0<c<10<c<1. In this case F12(n,b;c;z){{}_{2}F_{1}}(-n,b;c;z) has nn simple negative roots. See Figure 3 for an example of this type with n=2n=2. Figure 4 shows the configurations of two examples with n=5n=5.

  • n3n\geq 3 and 1<c<0-1<c<0, or n=3n=3 and 5/4<c<1-5/4<c<-1, or n=2n=2 and 1/2<c<0-1/2<c<0. In these case, F12(n,b;c;z){{}_{2}F_{1}}(-n,b;c;z) has n2n-2 simple negative roots, one root 0<z0<10<z_{0}<1, and another root 1/z0>11/z_{0}>1. Figure 5 shows the configurations of two examples with n=5n=5. ∎

Refer to caption
Figure 3. Genus 1 example with n=2n=2 and 0<c<10<c<1.
Refer to caption
c=0.001c=0.001
Refer to caption
c=0.5c=0.5
Figure 4. (5,1)(5,1) balanced configurations with 0<c<10<c<1. The circles and squares represent the necks at levels one and two respectively.
Refer to caption
c=0.5c=-0.5
Refer to caption
c=0.999c=-0.999
Figure 5. (5,1)(5,1) balanced configurations with 1<c<0-1<c<0. The circles and squares represent the necks at levels one and two respectively.
Remark 13.

Examples with six Scherk ends are parameterized by three real parameters, here by bb, cc, and the family parameter τ\tau. We see that the relation b+c=1nb+c=1-n imposes a rotational symmetry. It can be imagined that removing the relation would break this symmetry.

Remark 14.

The polynomial method is often used to find balanced configurations of interacting points in the plane. In minimal surface theory, it has been employed in many implementations of Traizet’s node-opening technique [Tra02b, Tra02a, TW05, Li12, CW12, Con17a, Con17b, CF22].

2.5. Surfaces with eight ends of type (1,n,1)

Theorem 5 generalizes to the following lemma with similar proof

Lemma 6.

If we fix ql±1,kq_{l\pm 1,k}’s and assume that cl=1c_{l}=1. Then ql,kq_{l,k}’s in a balanced configuration are given by the roots of a Stieltjes polynomial P(z)P(z) of degree nln_{l} that solves the generalized Lamé equation (a.k.a. second-order Fuchsian equation) [Mar66]

(14) P′′\displaystyle P^{\prime\prime} +(cz+k=1nl1cl1zql1,k+k=1nl+1cl+1zql+1,k)P\displaystyle+\Big{(}\frac{c}{z}+\sum_{k=1}^{n_{l-1}}\frac{-c_{l-1}}{z-q_{l-1,k}}+\sum_{k=1}^{n_{l+1}}\frac{-c_{l+1}}{z-q_{l+1,k}}\Big{)}P^{\prime}
+(γ0z+k=1nl1γl1,kzql1,k+k=1nl+1γl+1,kzql+1,k)P=0,\displaystyle+\Big{(}\frac{\gamma_{0}}{z}+\sum_{k=1}^{n_{l-1}}\frac{\gamma_{l-1,k}}{z-q_{l-1,k}}+\sum_{k=1}^{n_{l+1}}\frac{\gamma_{l+1,k}}{z-q_{l+1,k}}\Big{)}P=0,

where c=1+θ˙l+1,0θ˙l,0c=1+\dot{\theta}_{l+1,0}-\dot{\theta}_{l,0}, subject to conditions

γ0+k=1nl1γl1,k+k=1nl+1γl+1,k\displaystyle\gamma_{0}+\sum_{k=1}^{n_{l-1}}\gamma_{l-1,k}+\sum_{k=1}^{n_{l+1}}\gamma_{l+1,k} =0,\displaystyle=0,
k=1nl1γl1,kql1,k+k=1nl+1γl+1,kql+1,k.\displaystyle\sum_{k=1}^{n_{l-1}}\gamma_{l-1,k}q_{l-1,k}+\sum_{k=1}^{n_{l+1}}\gamma_{l+1,k}q_{l+1,k}. =:nlb,\displaystyle=:-n_{l}b,

and

cnl1cl1nl+1cl+1=1nl+b.c-n_{l-1}c_{l-1}-n_{l+1}c_{l+1}=1-n_{l}+b.

Moreover, the matrix (Fl,k/ql,j)1j,knl(\partial F_{l,k}/\partial q_{l,j})_{1\leq j,k\leq n_{l}} is nonsingular as long as bb is not a non-positive integer bigger than nln_{l}.

Indeed, a root of P(z)P(z) is simple if and only if it does not coincide with 0 or any ql±1,kq_{l\pm 1,k}. If the roots (ql,k)(q_{l,k}) of P(z)P(z) are all simple, then they solve the equations [Mar66]

1kjnl2ql,kql,j+1jnl+1cl+1ql,kql+1,j+1jnl1cl1ql,kql1,j+cql,k=Fl,kql,k=0,\sum_{1\leq k\neq j\leq n_{l}}\frac{2}{q_{l,k}-q_{l,j}}+\sum_{1\leq j\leq n_{l+1}}\frac{-c_{l+1}}{q_{l,k}-q_{l+1,j}}\\ +\sum_{1\leq j\leq n_{l-1}}\frac{-c_{l-1}}{q_{l,k}-q_{l-1,j}}+\frac{c}{q_{l,k}}=\frac{F_{l,k}}{q_{l,k}}=0,

which is exactly our balance condition; see Remark 4. Moreover, an equation system generalizing (13) has been obtained in [Hei78, §136], from which we may conclude the non-singularity of the Jacobian. In fact, there are

(nl1+nl+nl+11nl1+nl+11)\binom{n_{l-1}+n_{l}+n_{l+1}-1}{n_{l-1}+n_{l+1}-1}

choices of γ\gamma for which (14) has a polynomial solution of degree nln_{l} [Hei78, §135].

This observation allows us to easily construct balanced and rigid configurations of type (1,n,1)(1,n,1): Up to reparametrizations and complex scalings, we may assume that c2=1c_{2}=1 and q1,1=1q_{1,1}=1. Then q3,1q_{3,1} must be real, and (q2,k)1kn(q_{2,k})_{1\leq k\leq n} are given by roots of a Heun polynomial. Such a configuration depends locally on four real parameters, namely q3,1q_{3,1}, c1c_{1}, c3c_{3} and cc (or bb). When these are given, we have n+1n+1 Heun polynomials, each of which gives balanced positions of q2,kq_{2,k}’s. For each of the Heun polynomials PP, we have

θ˙2,0θ˙1,0\displaystyle\dot{\theta}_{2,0}-\dot{\theta}_{1,0} =P(1)P(1)c1,\displaystyle=\frac{P^{\prime}(1)}{P(1)}-c_{1},
θ˙3,0θ˙2,0\displaystyle\dot{\theta}_{3,0}-\dot{\theta}_{2,0} =c1=b+c1+c3n,\displaystyle=c-1=b+c_{1}+c_{3}-n,
θ˙4,0θ˙3,0\displaystyle\dot{\theta}_{4,0}-\dot{\theta}_{3,0} =P(q3,1)P(q3,1)c3.\displaystyle=\frac{P^{\prime}(q_{3,1})}{P(q_{3,1})}-c_{3}.

Together with the family parameter τ\tau, the surface depends locally on five parameters, which is expected because there are eight ends.

Example 3 (Symmetric examples).

When q3,1=q1,1=1q_{3,1}=q_{1,1}=1, the Heun polynomial reduces to a hypergeometric polynomial F12(n,b;c;z){{}_{2}F_{1}}(-n,b;c;z), where c1+c3=n1b+cc_{1}+c_{3}=n-1-b+c. Assume further that b+c=1nb+c=1-n, so c1+c3=2bc_{1}+c_{3}=-2b. This imposes a symmetry in the configuration. Because (c1+c3)P(1)/P(1)=nb(c_{1}+c_{3})P^{\prime}(1)/P(1)=-nb, the embeddedness conditions simplify to

c1>n/2,c3>n/2,1n/2<c<1,n<b<n/2.c_{1}>n/2,\quad c_{3}>n/2,\quad 1-n/2<c<1,\quad-n<b<-n/2.

As explained in Example 2, the hypergeometric polynomial has real roots if bb and cc lie in the blue regions of Figure 1. More specifically:

  • When n2n\geq 2 and 0<c<10<c<1, F12(n,b;c;z){{}_{2}F_{1}}(-n,b;c;z) has nn simple negative roots. See Figure 6 for an example with n=5n=5.

  • When n4n\geq 4 and 1<c<0-1<c<0, or n=3n=3 and 1/2<c<0-1/2<c<0, F12(n,b;c;z){{}_{2}F_{1}}(-n,b;c;z) has n2n-2 simple negative roots, one root 0<z0<10<z_{0}<1, and another root 1/z0>11/z_{0}>1. ∎

Refer to caption
Figure 6. Genus 4 example with n=5n=5 and 0<c<10<c<1.
Example 4 (Offset handles).

There are embedded examples in which the handles are not symmetrically placed. For instance, one balanced configuration of type (1,2,1)(1,2,1) is given by

q3,1=2/3,\displaystyle q_{3,1}=2/3, q2,1=1/3,\displaystyle q_{2,1}=-1/3, q2,2=23,\displaystyle q_{2,2}=-23,
c1=8/5,\displaystyle c_{1}=8/5, c3=4189/2890,\displaystyle c_{3}=4189/2890, b=9857/8670,\displaystyle b=-9857/8670,

so c=3956/4335c=3956/4335. ∎

2.6. Concatenating surfaces of type (1,n,1)

We describe a family of examples in the same spirit as [Tra02a, Proposition 2.3]. Assume that we are in possession of RR configurations of type (1,n(r),1)(1,n^{(r)},1), n(r)>1n^{(r)}>1, 1rR1\leq r\leq R. In the following, we use superscript (r)(r) to denote the parameters of the rr-th configuration. Up to reparameterizations and complex scalings, we may assume that c2(r)=1c_{2}^{(r)}=1 and q1,1(r)=1q_{1,1}^{(r)}=1. Then we may concatenate these configurations into one of type

(1,n2,1,n4,1,,1,n2R,1)(1,n_{2},1,n_{4},1,\cdots,1,n_{2R},1)

such that q1,1=1q_{1,1}=1, c1=1c_{1}=1, and for 1rR1\leq r\leq R, we have n2r=n(r)n_{2r}=n^{(r)},

q2r,k\displaystyle q_{2r,k} =q2r1,1q2,k(r),\displaystyle=q_{2r-1,1}q_{2,k}^{(r)}, q2r+1,1\displaystyle q_{2r+1,1} =q2r1,1q3,1(r),\displaystyle=q_{2r-1,1}q_{3,1}^{(r)},
c2r\displaystyle c_{2r} =c2r1/c1(r),\displaystyle=c_{2r-1}/c_{1}^{(r)}, c2r+1\displaystyle c_{2r+1} =c2r1c3(r)/c1(r),\displaystyle=c_{2r-1}c_{3}^{(r)}/c_{1}^{(r)},

and

θ˙2r+1,0θ˙2r,0=c2r(c(r)1).\dot{\theta}_{2r+1,0}-\dot{\theta}_{2r,0}=c_{2r}(c^{(r)}-1).

The balance of even layers then follows from the balance of each sub-configuration. The balance of odd layers leads to

θ˙2r,0θ˙2r1,0=c2r(θ˙2,0(r)θ˙1,0(r)+c1(r))+c2r2(θ˙4,0(r1)θ˙3,0(r1)+c3(r1))c2r1\dot{\theta}_{2r,0}-\dot{\theta}_{2r-1,0}=c_{2r}(\dot{\theta}_{2,0}^{(r)}-\dot{\theta}_{1,0}^{(r)}+c_{1}^{(r)})+c_{2r-2}(\dot{\theta}_{4,0}^{(r-1)}-\dot{\theta}_{3,0}^{(r-1)}+c_{3}^{(r-1)})-c_{2r-1}

for 1rR+11\leq r\leq R+1. As expected, such a configuration depends locally on 4R4R real parameters, namely q3,1(r)q_{3,1}^{(r)}, c1(r)c_{1}^{(r)}, c3(r)c_{3}^{(r)}, and c(r)c^{(r)}, 1rR1\leq r\leq R.

We may impose symmetry by assuming that q3,1(r)=1q_{3,1}^{(r)}=1, so q2r+1,1=1q_{2r+1,1}=1 for all 0rR0\leq r\leq R, and that b(r)+c(r)=1n(r)b^{(r)}+c^{(r)}=1-n^{(r)}, so c1(r)+c3(r)=n(r)1b(r)+c(r)=2b(r)c_{1}^{(r)}+c_{3}^{(r)}=n^{(r)}-1-b^{(r)}+c^{(r)}=-2b^{(r)}. Then q2r,k=q2,k(r)q_{2r,k}=q_{2,k}^{(r)}, 1kn(r)1\leq k\leq n^{(r)}, are given by the roots of F12(n(r),b(r);c(r);z){{}_{2}F_{1}}(-n^{(r)},b^{(r)};c^{(r)};z), 1rR1\leq r\leq R. Because

θ˙2,0(r)θ˙1,0(r)+c1(r)=θ˙4,0(r)θ˙3,0(r)+c1(r)=n(r)/2,\dot{\theta}_{2,0}^{(r)}-\dot{\theta}_{1,0}^{(r)}+c_{1}^{(r)}=\dot{\theta}_{4,0}^{(r)}-\dot{\theta}_{3,0}^{(r)}+c_{1}^{(r)}=n^{(r)}/2,

the embeddedness conditions simplify to

2nlcl>nl1cl1+nl+1cl+12n_{l}c_{l}>n_{l-1}c_{l-1}+n_{l+1}c_{l+1}

for 1lL1\leq l\leq L under the condition that n0=nL+1=0n_{0}=n_{L+1}=0. That is, the sequence (nlcl)1lL(n_{l}c_{l})_{1\leq l\leq L} must be concave. For even ll, the concavity implies that b(r)>nb^{(r)}>-n hence c(r)<1c^{(r)}<1 for all 1rR1\leq r\leq R. We may choose, for instance, nlcl=ln(1+l)n_{l}c_{l}=\ln(1+l) or nlcl=(expl1)/exp(l1)n_{l}c_{l}=(\exp l-1)/\exp(l-1) to obtain embedded minimal surfaces.

Remark 15.

We can also append a configuration of type (1,n(r))(1,n^{(r)}) to the sequence of (1,n(r),1)(1,n^{(r)},1)-configurations to obtain a configuration of type

(1,n2,1,n4,1,,1,n2R2,1,n2R),(1,n_{2},1,n_{4},1,\ldots,1,n_{2R-2},1,n_{2R}),

where the ql,k,cl,θ˙l,0q_{l,k},c_{l},\dot{\theta}_{l,0} terms are defined as above. Therefore, an embedded example of any genus with any even number (>2>2) of ends can be constructed.

2.7. Numerical examples

The balance equations can be combined into one differential equation that is much easier to solve. A solution of this differential equation corresponds to a lot of balance configurations that are equivalent by permuting the locations of the nodes.

Lemma 7.

Let LL be a positive integer, n1,n2,,nLn_{1},n_{2},\ldots,n_{L}\in\mathbb{N}, and suppose {ql,k}\{q_{l,k}\} is a configuration such that the ql,kq_{l,k} are distinct. Let

Pl(z)=k=1nl(zql,k),P(z)=l=1LPl(z),P0(z)=PL+1(z)=1,P_{l}(z)=\prod_{k=1}^{n_{l}}(z-q_{l,k}),\quad P(z)=\prod_{l=1}^{L}P_{l}(z),\quad P_{0}(z)=P_{L+1}(z)=1,\\

and

P(z)=l=1L(cl2zPl′′(z)P(z)Pl(z)clcl+1zPl(z)Pl+1(z)P(z)Pl(z)Pl+1(z)+(cl2+cl(θ˙l+1,0θ˙l,0))Pl(z)P(z)Pl(z)).\begin{split}\mathcal{F}P(z)=\sum_{l=1}^{L}&\left(\frac{c_{l}^{2}zP_{l}^{\prime\prime}(z)P(z)}{P_{l}(z)}-\frac{c_{l}c_{l+1}zP_{l}^{\prime}(z)P_{l+1}^{\prime}(z)P(z)}{P_{l}(z)P_{l+1}(z)}\right.\\ &\hskip 14.45377pt\left.+\left(c_{l}^{2}+c_{l}(\dot{\theta}_{l+1,0}-\dot{\theta}_{l,0})\right)\frac{P_{l}^{\prime}(z)P(z)}{P_{l}(z)}\right).\end{split}

Then the configuration {ql,k}\{q_{l,k}\} is balanced if and only if P(z)0\mathcal{F}P(z)\equiv 0.

Proof.

We have seen that,

Pl′′(ql,k)Pl(ql,k)=1kjnl2ql,kql,j,Pl±1(ql,k)Pl±1(ql,k)=j=1nl±11ql,kql±1,j.\frac{P_{l}^{\prime\prime}(q_{l,k})}{P^{\prime}_{l}(q_{l,k})}=\sum_{1\leq k\neq j\leq n_{l}}\frac{2}{q_{l,k}-q_{l,j}},\qquad\frac{P_{l\pm 1}^{\prime}(q_{l,k})}{P_{l\pm 1}(q_{l,k})}=\sum_{j=1}^{n_{l\pm 1}}\frac{1}{q_{l,k}-q_{l\pm 1,j}}.

Define

Fl(z)=cl2zPl′′(z)Pl(z)clcl+1zPl+1(z)Pl+1(z)clcl1zPl1(z)Pl1(z)+cl2+cl(θ˙l+1,0θ˙l,0).F_{l}(z)=\frac{c_{l}^{2}zP_{l}^{\prime\prime}(z)}{P_{l}^{\prime}(z)}-\frac{c_{l}c_{l+1}zP_{l+1}^{\prime}(z)}{P_{l+1}(z)}-\frac{c_{l}c_{l-1}zP_{l-1}^{\prime}(z)}{P_{l-1}(z)}+c_{l}^{2}+c_{l}(\dot{\theta}_{l+1,0}-\dot{\theta}_{l,0}).

Then Fl,k=Fl(ql,k)F_{l,k}=F_{l}(q_{l,k}). Set

Ql(z)=Pl(z)P(z)Pl(z)Fl(z)=cl2zPl′′(z)P(z)Pl(z)clcl+1zPl(z)Pl+1(z)P(z)Pl(z)Pl+1(z)clcl1zPl1(z)Pl(z)P(z)Pl1(z)Pl(z)+(cl2+cl(θ˙l+1,0θ˙l,0))Pl(z)P(z)Pl(z).\begin{split}Q_{l}(z)&=\frac{P_{l}^{\prime}(z)P(z)}{P_{l}(z)}F_{l}(z)\\ &=\frac{c_{l}^{2}zP_{l}^{\prime\prime}(z)P(z)}{P_{l}(z)}-\frac{c_{l}c_{l+1}zP_{l}^{\prime}(z)P_{l+1}^{\prime}(z)P(z)}{P_{l}(z)P_{l+1}(z)}-\frac{c_{l}c_{l-1}zP_{l-1}^{\prime}(z)P_{l}^{\prime}(z)P(z)}{P_{l-1}(z)P_{l}(z)}\\ &\hskip 14.45377pt+\left(c_{l}^{2}+c_{l}(\dot{\theta}_{l+1,0}-\dot{\theta}_{l,0})\right)\frac{P_{l}^{\prime}(z)P(z)}{P_{l}(z)}.\end{split}

Then Fl,k=0F_{l,k}=0 if and only if Ql(ql,k)=0Q_{l}(q_{l,k})=0.

Now observe that Ql(z)Q_{l}(z) and Q(z)=P(z)Q(z)=\mathcal{F}P(z) are polynomials with degree strictly less than

degP=N=l=1Lnl,\deg P=N=\sum_{l=1}^{L}n_{l},

and Q(ql,k)=Ql(ql,k)Q(q_{l,k})=Q_{l}(q_{l,k}) for 1knl1\leq k\leq n_{l} and 1lL1\leq l\leq L. If Q0Q\equiv 0 then Ql(ql,k)=0Q_{l}(q_{l,k})=0 and so {ql,k}\{q_{l,k}\} is a balanced configuration. If {ql,k}\{q_{l,k}\} is a balanced configuration then Q(ql,k)=Ql(ql,k)=Fl,k=0Q(q_{l,k})=Q_{l}(q_{l,k})=F_{l,k}=0. Hence, QQ has at least NN distinct roots. Since the degree of QQ is strictly less than NN, we must have Q0Q\equiv 0. ∎

It is relatively easy to numerically solve P(z)0\mathcal{F}P(z)\equiv 0 as long as we don’t have too many levels and necks. So we use this lemma to find balanced configurations. Since all previous examples admit a horizontal reflection symmetry, we are most interested examples without this symmetry, or with no non-trivial symmetry at all.

Figure 7 shows an example with L=3L=3,

n1=1,n2=3,n3=2\displaystyle n_{1}=1,n_{2}=3,n_{3}=2
c1=2,c2=1,c3=13/16\displaystyle c_{1}=2,c_{2}=1,c_{3}=13/16
θ1,0=0,θ2,0=1/2,θ3,0=27/16,θ4,0=29/16.\displaystyle\theta_{1,0}=0,\theta_{2,0}=-1/2,\theta_{3,0}=-27/16,\theta_{4,0}=-29/16.

This configuration corresponds to an embedded minimal surface with eight ends and genus three in the quotient. It has no horizontal reflectional symmetry, but does have a rotational symmetry.

Refer to caption
Refer to caption
Figure 7. A (1,3,2)(1,3,2) balanced configuration with no horizontal reflectional symmetry. The circles, squares, and diamonds represent the necks at levels one, two, and three respectively.

Figure 8 shows two examples with L=3L=3,

n1=1,n2=4,n3=3\displaystyle n_{1}=1,n_{2}=4,n_{3}=3
c1=7/2,c2=1,c3=3/4\displaystyle c_{1}=7/2,c_{2}=1,c_{3}=3/4
θ1,0=0,θ2,0=2,θ3,0=13/5,θ4,0=541/180.\displaystyle\theta_{1,0}=0,\theta_{2,0}=-2,\theta_{3,0}=-13/5,\theta_{4,0}=-541/180.

These configurations correspond to embedded minimal surfaces with eight ends and genus five in the quotient, with no nontrivial symmetry.

Refer to caption
Refer to caption
Figure 8. (1,4,3)(1,4,3) balanced configurations with no symmetries. The circles, squares, and diamonds represent the necks at levels one, two, and three respectively.

Figure 9 shows two examples with L=3L=3,

n1=1,n2=7,n3=3,\displaystyle n_{1}=1,n_{2}=7,n_{3}=3,
c1=17/7,c2=1,c3=3/2,\displaystyle c_{1}=17/7,c_{2}=1,c_{3}=3/2,
θ1,0=0,θ2,0=1/2,θ3,0=3/2,θ4,0=2468/441.\displaystyle\theta_{1,0}=0,\theta_{2,0}=-1/2,\theta_{3,0}=-3/2,\theta_{4,0}=-2468/441.

These configurations correspond to embedded minimal surfaces with eight ends and genus eight in the quotient, with no nontrivial symmetry.

Refer to caption
Refer to caption
Figure 9. (1,7,3)(1,7,3) balanced configurations with no symmetries. The circles, squares, and diamonds represent the necks at levels one, two, and three respectively.

3. Construction

3.1. Opening nodes

To each vertical plane is associated a punctured complex plane l×{0}\mathbb{C}^{\times}_{l}\simeq\mathbb{C}\setminus\{0\}, 1lL+11\leq l\leq L+1. They can be seen as Riemann spheres ^l{}\hat{\mathbb{C}}_{l}\simeq\mathbb{C}\cup\{\infty\} with two fixed punctures at pl,0=0p_{l,0}=0 and pl,=p_{l,\infty}=\infty, corresponding to the two ends.

To each neck is associated a puncture pl,kl×p^{\circ}_{l,k}\in\mathbb{C}^{\times}_{l} and a puncture pl,kl+1×p^{\prime\circ}_{l,k}\in\mathbb{C}^{\times}_{l+1}. Our initial surface at τ=0\tau=0 is the noded Riemann surface Σ0\Sigma_{0} obtained by identifying pl,kp^{\circ}_{l,k} and pl,kp^{\prime\circ}_{l,k} for 1lL1\leq l\leq L and 1knl1\leq k\leq n_{l}.

As τ\tau increases, we open the nodes into necks as follows: Fix local coordinates wl,0=zw_{l,0}=z in the neighborhood of 0^l0\in\hat{\mathbb{C}}_{l} and wl,=1/zw_{l,\infty}=1/z in the neighborhood of ^l\infty\in\hat{\mathbb{C}}_{l}. For each neck, we consider parameters (pl,k,pl,k)(p_{l,k},p^{\prime}_{l,k}) in the neighborhoods of (pl,k,pl,k)(p^{\circ}_{l,k},p^{\prime\circ}_{l,k}) and local coordinates

wl,k=ln(z/pl,k)andwl,k=ln(z/pl,k)w_{l,k}=\ln(z/p_{l,k})\quad\text{and}\quad w^{\prime}_{l,k}=\ln(z/p^{\prime}_{l,k})

in a neighborhood of pl,kp_{l,k} and pl,kp^{\prime}_{l,k}, respectively. In this paper, the branch cut of ln(z)\ln(z) is along the negative real axis, and we use the principal value of ln(z)\ln(z) with imaginary part in the interval (π,π](-\pi,\pi].

As we only open finitely many necks, we may choose δ>0\delta>0 independent of kk and ll such that the disks

|wh|<2δ,h𝖧(=[1,L+1]×{0,}),\displaystyle|w_{h}|<2\delta,\qquad h\in\mathsf{H}\quad(=[1,L+1]\times\{0,\infty\}),
|wl,k|<2δand|wl,k|<2δ,1lL,1knk\displaystyle|w_{l,k}|<2\delta\quad\text{and}\quad|w^{\prime}_{l,k}|<2\delta,\qquad 1\leq l\leq L,1\leq k\leq n_{k}

are all disjoint. For parameters t=(tl,k)1lL,1knlt=(t_{l,k})_{1\leq l\leq L,1\leq k\leq n_{l}} in a neighborhood of 0 with |tl,k|<δ2|t_{l,k}|<\delta^{2}, we remove the disks

|wl,k|<|tl,k|/δand|wl,k|<|tl,k|/δ|w_{l,k}|<|t_{l,k}|/\delta\quad\text{and}\quad|w^{\prime}_{l,k}|<|t_{l,k}|/\delta

and identify the annuli

|tl,k|/δ|wl,k|δand|tl,k|/δ|wl,k|δ|t_{l,k}|/\delta\leq|w_{l,k}|\leq\delta\quad\text{and}\quad|t_{l,k}|/\delta\leq|w^{\prime}_{l,k}|\leq\delta

by

wl,kwl,k=tl,k.w_{l,k}w^{\prime}_{l,k}=t_{l,k}.

If tl,k0t_{l,k}\neq 0 for all 1lL1\leq l\leq L and 1knl1\leq k\leq n_{l}, we obtain a Riemann surface denoted by Σt\Sigma_{t}.

3.2. Weierstrass data

We construct a conformal minimal immersion using the Weierstrass parameterization in the form

zRez(Φ1,Φ2,Φ3),z\mapsto\operatorname{Re}\int^{z}(\Phi_{1},\Phi_{2},\Phi_{3}),

where Φi\Phi_{i} are meromorphic 1-forms on Σt\Sigma_{t} satisfying the conformality equation

(15) Q:=Φ12+Φ22+Φ32=0.Q:=\Phi_{1}^{2}+\Phi_{2}^{2}+\Phi_{3}^{2}=0.

3.2.1. A-periods

We consider the following fixed domains in all Σt\Sigma_{t}:

Ul,δ={z^v:\displaystyle U_{l,\delta}=\{z\in\hat{\mathbb{C}}_{v}\colon |wl,k(z)|>δ/21knlif 1lL\displaystyle|w^{\circ}_{l,k}(z)|>\delta/2\quad\forall 1\leq k\leq n_{l}\quad\text{if}\;1\leq l\leq L
and |wl,k(z)|>δ/21knl1if 2lL+1}\displaystyle|w^{\prime\circ}_{l,k}(z)|>\delta/2\quad\forall 1\leq k\leq n_{l-1}\quad\text{if}\;2\leq l\leq L+1\}

and Uδ=1lLUl,δU_{\delta}=\bigsqcup_{1\leq l\leq L}U_{l,\delta}.

Let Al,kA_{l,k} denote a small counterclockwise circle in Ul,δU_{l,\delta} around pl,kp_{l,k}; it is then homologous in Σt\Sigma_{t} to a clockwise circle in Ul+1,δU_{l+1,\delta} around pl,kp^{\prime}_{l,k}. Moreover, let Al,0A_{l,0} (resp. Al,A_{l,\infty}) denote a small counterclockwise circle in Ul,δU_{l,\delta} around 0 (resp. \infty).

Recall that the vertical period vector is assumed to be (0,0,2π)(0,0,2\pi), so we need to solve the A-period problems

ReAh(Φ1,Φ2,Φ3)=(0,0,2πσh)andReAl,k(Φ1,Φ2,Φ3)=(0,0,0)\operatorname{Re}\int_{A_{h}}(\Phi_{1},\Phi_{2},\Phi_{3})=(0,0,2\pi\sigma_{h})\quad\text{and}\quad\operatorname{Re}\int_{A_{l,k}}(\Phi_{1},\Phi_{2},\Phi_{3})=(0,0,0)

for h𝖧h\in\mathsf{H}, 1lL1\leq l\leq L, and 1knl1\leq k\leq n_{l}. Here, the orientation σh=±1\sigma_{h}=\pm 1 satisfies

σh=σς(h),\sigma_{h}=-\sigma_{\varsigma(h)},

where the “counterclockwise rotation” ς\varsigma on 𝖧\mathsf{H} is defined by

(16) {ς(0l)=0l1,2lL+1,ς(01)=1,ς(l)=l+1,1lL,ς(L+1)=0L+1.\begin{cases}\varsigma(0_{l})=0_{l-1},&2\leq l\leq L+1,\\ \varsigma(0_{1})=\infty_{1},\\ \varsigma(\infty_{l})=\infty_{l+1},&1\leq l\leq L,\\ \varsigma(\infty_{L+1})=0_{L+1}.\end{cases}

In particular, we have σl,0=σl,\sigma_{l,0}=-\sigma_{l,\infty} for all 1lL+11\leq l\leq L+1.

Recall that the surface tends to an (L+1)(L+1)-sheeted xzxz-plane in the limit τ0\tau\to 0. So we define the meromorphic functions Φ1\Phi_{1}, Φ2\Phi_{2} and Φ3\Phi_{3} as the unique regular 1-forms on Σt\Sigma_{t} (see [Tra13, §8]) with simple poles at php_{h}, h𝖧h\in\mathsf{H}, and the A-periods

Ah(Φ1,Φ~2,Φ3)\displaystyle\int_{A_{h}}{(\Phi_{1},\widetilde{\Phi}_{2},\Phi_{3})} =2πi(αh,βh,γhiσh),\displaystyle=2\pi{\rm i}(\alpha_{h},\beta_{h},\gamma_{h}-{\rm i}\sigma_{h}), h𝖧,\displaystyle h\in\mathsf{H},
Al,k(Φ1,Φ~2,Φ3)\displaystyle\int_{A_{l,k}}(\Phi_{1},\widetilde{\Phi}_{2},\Phi_{3}) =2πi(αl,k,βl,k,γl,k),\displaystyle=2\pi{\rm i}(\alpha_{l,k},\beta_{l,k},\gamma_{l,k}), 1lL,1knl,\displaystyle 1\leq l\leq L,1\leq k\leq n_{l},

where Φ2=τΦ~2\Phi_{2}=\tau\widetilde{\Phi}_{2} and, by Residue Theorem, it is necessary that

(17) αl,0+αl,+1knlαl,k1knl1αl1,k\displaystyle\alpha_{l,0}+\alpha_{l,\infty}+\sum_{1\leq k\leq n_{l}}\alpha_{l,k}-\sum_{1\leq k\leq n_{l-1}}\alpha_{l-1,k} =0,\displaystyle=0,
(18) βl,0+βl,+1knlβl,k1knl1βl1,k\displaystyle\beta_{l,0}+\beta_{l,\infty}+\sum_{1\leq k\leq n_{l}}\beta_{l,k}-\sum_{1\leq k\leq n_{l-1}}\beta_{l-1,k} =0,\displaystyle=0,
(19) γl,0+γl,+1knlγl,k1knl1γl1,k\displaystyle\gamma_{l,0}+\gamma_{l,\infty}+\sum_{1\leq k\leq n_{l}}\gamma_{l,k}-\sum_{1\leq k\leq n_{l-1}}\gamma_{l-1,k} =0,\displaystyle=0,

for 1lL+11\leq l\leq L+1. Then the A-period problems are solved by definition.

3.2.2. Balance of ends

Summing up (18) over ll gives

(20) h𝖧βh=0,\sum_{h\in\mathsf{H}}\beta_{h}=0,

which we use to replace Equation (18) with l=L+1l=L+1.

In this paper, the punctures pl,0p_{l,0} and pl,p_{l,\infty} correspond to Scherk-type ends. Hence we fix

(21) αh2+τ2βh21andγh0\alpha^{2}_{h}+\tau^{2}\beta_{h}^{2}\equiv 1\quad\text{and}\quad\gamma_{h}\equiv 0

for all h𝖧h\in\mathsf{H}, so that (the stereographic projection of) the Gauss map G=(Φ1+iΦ2)/Φ3G=-(\Phi_{1}+{\rm i}\Phi_{2})/\Phi_{3} extends holomorphically to the punctures php_{h} with unitary values. Then Equations (19) are not independent: if it is solved for 1lL1\leq l\leq L, it is automatically solved for l=L+1l=L+1.

In particular, at τ=0\tau=0, we have αh2=1\alpha_{h}^{2}=1. In view of the orientation of the ends, we choose αl,0=1\alpha_{l,0}=1 and αl,=1\alpha_{l,\infty}=-1 so that G(pl,)=G(pl,0)=iσl,0G(p_{l,\infty})=G(p_{l,0})={\rm i}\sigma_{l,0}.

Summing up (17) over ll gives

(22) 1lL+1(1τ2βl,21τ2βl,02)=0,\sum_{1\leq l\leq L+1}\Big{(}\sqrt{1-\tau^{2}\beta_{l,\infty}^{2}}-\sqrt{1-\tau^{2}\beta_{l,0}^{2}}\Big{)}=0,

which we use to replace Equation (17) with l=L+1l=L+1.

Remark 16.

The conditions (20) and (22) are disguises of the balance condition of Scherk ends, namely that the unit vectors in their directions should sum up to 0.

3.2.3. B-periods

For 1lL+11\leq l\leq L+1, we fix a point OlUl,δO_{l}\in U_{l,\delta}. For every 1lL1\leq l\leq L and 1knl1\leq k\leq n_{l} and tl,k0t_{l,k}\neq 0, let Bl,kB_{l,k} be the concatenation of

  1. (1)

    a path in Ul,δU_{l,\delta} from OlO_{l} to wl,k=δw_{l,k}=\delta,

  2. (2)

    the path parameterized by wl,k=δ12stl,ksw_{l,k}=\delta^{1-2s}\,t_{l,k}^{s} for s[0,1]s\in[0,1], from wl,k=δw_{l,k}=\delta to wl,k=th/δw_{l,k}=t_{h}/\delta, which is identified with wl,k=δw^{\prime}_{l,k}=\delta, and

  3. (3)

    a path in Ul+1,δU_{l+1,\delta} from wl,k=δw^{\prime}_{l,k}=\delta to Ol+1O_{l+1}.

We need to solve the B-period problem, namely that

(23) ReBl,k(Φ1,Φ2,Φ3)=ReBl,1(Φ1,Φ2,Φ3).\operatorname{Re}\int_{B_{l,k}}(\Phi_{1},\Phi_{2},\Phi_{3})=\operatorname{Re}\int_{B_{l,1}}(\Phi_{1},\Phi_{2},\Phi_{3}).

3.2.4. Conformality

Lemma 8.

For tt sufficiently close to 0, the conformality condition (15) is equivalent to

(24) 𝔊l,k:=Al,kwl,kQdwl,k\displaystyle\mathfrak{G}_{l,k}:=\int_{A_{l,k}}\frac{w_{l,k}Q}{dw_{l,k}} =0,1lL,1knl,\displaystyle=0,\quad 1\leq l\leq L,\quad 1\leq k\leq n_{l},
(25) 𝔉l,k:=Al,kQdwl,k\displaystyle\mathfrak{F}_{l,k}:=\int_{A_{l,k}}\frac{Q}{dw_{l,k}} =0,1lL,2knl,\displaystyle=0,\quad 1\leq l\leq L,\quad 2\leq k\leq n_{l},
(26) 𝔉l,k:=Al,kQdwl,k\displaystyle\mathfrak{F}^{\prime}_{l,k}:=\int_{A^{\prime}_{l,k}}\frac{Q}{dw^{\prime}_{l,k}} =0,1lL,1+δl,Lknl,\displaystyle=0,\quad 1\leq l\leq L,\quad 1+\delta_{l,L}\leq k\leq n_{l},

where Al,kA^{\prime}_{l,k} in (26) denotes a small counterclockwise circle in Ul+1,δU_{l+1,\delta} around pl,kp^{\prime}_{l,k} (hence homologous to Al,k-A_{l,k}), and δl,L=1\delta_{l,L}=1 if l=Ll=L and 0 otherwise.

Proof.

By our choice of αh\alpha_{h} and γh\gamma_{h}, the quadratic differential QQ has at most simple poles at the 2L+22L+2 punctures php_{h}, h𝖧h\in\mathsf{H}. The space of such quadratic differentials is of complex dimension 3(NL)3+(2L+2)=3NL13(N-L)-3+(2L+2)=3N-L-1. We will prove that

Q(𝔊,𝔉,𝔉)Q\mapsto(\mathfrak{G},\mathfrak{F},\mathfrak{F}^{\prime})

is an isomorphism. We prove the claim at t=0t=0; then the claim follows by continuity.

Consider QQ in the kernel. Recall from [Tra08] that a regular quadratic differential on Σ0\Sigma_{0} has at most double poles at the nodes pl,kp_{l,k} and pl,kp^{\prime}_{l,k}. Then (24) guarantees that QQ has at most simple poles at the nodes. By (25) and (26), QQ may only have simple poles at pl,1l×p_{l,1}\in\mathbb{C}^{\times}_{l}, 1lL1\leq l\leq L, and pL,1L+1×p^{\prime}_{L,1}\in\mathbb{C}^{\times}_{L+1}. So, on each Riemann sphere ^l\hat{\mathbb{C}}_{l}, QQ is a quadratic differential with at most simple poles at three punctures; the other two being 0, \infty. But such a quadratic differential must be 0. ∎

3.3. Using the Implicit Function Theorem

All parameters varies in a neighborhood of their central values, denoted by a superscript \circ. We will see that

βh=θ˙h,αl,k=γl,k=0,βl,k=cl,pl,k=pl,k¯.\beta^{\circ}_{h}=\dot{\theta}_{h},\;\alpha^{\circ}_{l,k}=\gamma^{\circ}_{l,k}=0,\;\beta^{\circ}_{l,k}=-c_{l},\;p^{\prime\circ}_{l,k}=\overline{p_{l,k}}.

Let us first solve Equations (20) and (22).

Proposition 9.

Given a configuration (q,θ˙)(q,\dot{\theta}) such that Θ1=Θ2=0\Theta_{1}=\Theta_{2}=0. For τ\tau sufficiently small and βh\beta_{h} close to βh=θ˙h\beta^{\circ}_{h}=\dot{\theta}_{h}, the solutions (τ,β)(\tau,\beta) to Equations (20) and (22) form a smooth manifold of dimension 2L+12L+1.

Proof.

At τ=0\tau=0, Equation (20) is solved by βh=θ˙h\beta^{\circ}_{h}=\dot{\theta}_{h} if Θ1=0\Theta_{1}=0. Taking the derivative of (22) with respect to τ2\tau^{2} gives

(27) 1lL+1βl,2βl,022=0,\sum_{1\leq l\leq L+1}\frac{\beta_{l,\infty}^{2}-\beta_{l,0}^{2}}{2}=0,

which is solved by βh=θ˙h\beta^{\circ}_{h}=\dot{\theta}_{h} if Θ2=0\Theta_{2}=0. The proposition then follows from Lemma 1 and the Implicit Function Theorem. ∎

From now on, we assume that the parameters (τ,(βh)h𝖧)(\tau,(\beta_{h})_{h\in\mathsf{H}}) are solutions to Equations (20) and (22) in a neighborhood of (0,θ˙)(0,\dot{\theta}).

3.3.1. Solving conformality problems

Proposition 10.

For τ\tau sufficiently small and βl,k\beta_{l,k}, pl,kp_{l,k}, and pl,kp^{\prime}_{l,k} in a neighborhood of their central values, there exist unique values of tl,kt_{l,k}, αl,k\alpha_{l,k}, and γl,k\gamma_{l,k}, depending real-analytically on (τ2,β,p,p)(\tau^{2},\beta,p,p^{\prime}), such that the balance equations (17) and (19) with 1lL1\leq l\leq L and the conformality Equations (24) and (25) are solved. Moreover, at τ=0\tau=0, we have tl,k=0t_{l,k}=0, αl,k=γl,k=0\alpha_{l,k}=\gamma_{l,k}=0,

tl,k(τ2)=14βl,k2,\frac{\partial t_{l,k}}{\partial(\tau^{2})}=\frac{1}{4}\beta_{l,k}^{2},

and, for 2knl2\leq k\leq n_{l},

(28) (τ2)(αl,kiσl,0γl,k)=12Res(Φ~22dwl,k,pl,k)=12Res(zΦ~22dz,pl,k).\frac{\partial}{\partial(\tau^{2})}(\alpha_{l,k}-{\rm i}\sigma_{l,0}\gamma_{l,k})=-\frac{1}{2}\operatorname{Res}\left(\frac{\widetilde{\Phi}_{2}^{2}}{dw_{l,k}},p_{l,k}\right)=-\frac{1}{2}\operatorname{Res}\left(\frac{z\widetilde{\Phi}_{2}^{2}}{dz},p_{l,k}\right).

Note that, according to this proposition, if βl,k0\beta^{\circ}_{l,k}\neq 0, then tl,k>0t_{l,k}>0 for sufficiently small τ\tau.

Proof.

At τ=0\tau=0, for 2knl2\leq k\leq n_{l} we have

𝔊l,k=Al,kwl,kQdwl,k=2πi(αl,k2+γl,k2)=0\mathfrak{G}_{l,k}=\int_{A_{l,k}}\frac{w_{l,k}Q}{dw_{l,k}}=2\pi{\rm i}(\alpha_{l,k}^{2}+\gamma_{l,k}^{2})=0

which vanishes when

αl,k=γl,k=0.\alpha_{l,k}=\gamma_{l,k}=0.

Recall that αh=±1\alpha_{h}=\pm 1 at τ=0\tau=0 and that γh0\gamma_{h}\equiv 0. Then by Residue Theorem, we have

αl,1=γl,1=0.\alpha_{l,1}=\gamma_{l,1}=0.

As a consequence, we have at τ=0\tau=0

Φ1=dz/z,Φ2=0,andΦ3=iσl,0dz/z,\Phi^{\circ}_{1}=dz/z,\quad\Phi^{\circ}_{2}=0,\quad\text{and}\quad\Phi^{\circ}_{3}=-{\rm i}\sigma_{l,0}dz/z,

so Q=0Q=0 as we expect.

We then compute the partial derivatives at τ=0\tau=0

αl,k𝔉l,k\displaystyle\frac{\partial}{\partial\alpha_{l,k}}\mathfrak{F}_{l,k} =Al,k2Φ1dwl,kΦ1αl,k|τ=0=Al,k2dz/zdz/pdzzpl,k=4πi,\displaystyle=\int_{A_{l,k}}2\frac{\Phi^{\circ}_{1}}{dw_{l,k}}\frac{\partial\Phi_{1}}{\partial\alpha_{l,k}}\bigg{|}_{\tau=0}=\int_{A_{l,k}}2\frac{dz/z}{dz/p}\frac{dz}{z-p_{l,k}}=4\pi{\rm i}\,,
γl,k𝔉l,k\displaystyle\frac{\partial}{\partial\gamma_{l,k}}\mathfrak{F}_{l,k} =Al,k2Φ3dwl,kΦ3γl,k|τ=0=Al,k2iσl,0dz/zdz/pdzzpl,k=4πσl,0,\displaystyle=\int_{A_{l,k}}2\frac{\Phi^{\circ}_{3}}{dw_{l,k}}\frac{\partial\Phi_{3}}{\partial\gamma_{l,k}}\bigg{|}_{\tau=0}=\int_{A_{l,k}}-2i\sigma_{l,0}\frac{dz/z}{dz/p}\frac{dz}{z-p_{l,k}}=4\pi\sigma_{l,0}\,,
tl,k𝔊l,k\displaystyle\frac{\partial}{\partial t_{l,k}}\mathfrak{G}_{l,k} =Al,k2wl,kdwl,k(Φ1Φ1tl,k+Φ3Φ3tl,k)\displaystyle=\int_{A_{l,k}}\frac{2w_{l,k}}{dw_{l,k}}\Big{(}\Phi^{\circ}_{1}\frac{\partial\Phi^{\circ}_{1}}{\partial t_{l,k}}+\Phi^{\circ}_{3}\frac{\partial\Phi^{\circ}_{3}}{\partial t_{l,k}}\Big{)}
=1πi(Al,kΦ1wl,kAl,kΦ1wl,k+Al,kΦ3wl,kAl,kΦ3wl,k)[Tra08, Lemma 3]\displaystyle=\frac{-1}{\pi{\rm i}}\Big{(}\int_{A_{l,k}}\frac{\Phi^{\circ}_{1}}{w_{l,k}}\int_{A^{\prime}_{l,k}}\frac{\Phi^{\circ}_{1}}{w^{\prime}_{l,k}}+\int_{A_{l,k}}\frac{\Phi^{\circ}_{3}}{w_{l,k}}\int_{A^{\prime}_{l,k}}\frac{\Phi^{\circ}_{3}}{w^{\prime}_{l,k}}\Big{)}\quad\text{\cite[cite]{[\@@bibref{}{traizet2008}{}{}, Lemma~{}3]}}
=8πi.\displaystyle=-8\pi{\rm i}.

All other partial derivatives vanish. Therefore, by the Implicit Function Theorem, there exist unique values of αl,k\alpha_{l,k}, γl,k\gamma_{l,k} (with 2knl2\leq k\leq n_{l}), and tl,kt_{l,k} (with 1knl1\leq k\leq n_{l}) that solve the conformality Equations (24) and (25). Recall that αh\alpha_{h} are determined by (21). Then αl,1\alpha_{l,1} and γl,1\gamma_{l,1} are uniquely determined by the linear balance equations (17) and (19).

Moreover,

(τ2)𝔉l,k=Al,kΦ~22dwl,k,(τ2)𝔊l,k=2πiβl,k2.\frac{\partial}{\partial(\tau^{2})}\mathfrak{F}_{l,k}=\int_{A_{l,k}}\frac{\widetilde{\Phi}_{2}^{2}}{dw_{l,k}},\quad\frac{\partial}{\partial(\tau^{2})}\mathfrak{G}_{l,k}=2\pi{\rm i}\beta_{l,k}^{2}.

Hence the total derivatives

dd(τ2)𝔉l,k=4πiαl,k(τ2)+4πσl,0γl,k(τ2)+2πiRes(Φ~22dwl,k,pl,k)=0\frac{d}{d(\tau^{2})}\mathfrak{F}_{l,k}=4\pi{\rm i}\frac{\partial\alpha_{l,k}}{\partial(\tau^{2})}+4\pi\sigma_{l,0}\frac{\partial\gamma_{l,k}}{\partial(\tau^{2})}+2\pi{\rm i}\operatorname{Res}\left(\frac{\widetilde{\Phi}_{2}^{2}}{dw_{l,k}},p_{l,k}\right)=0

and

dd(τ2)Al,k𝔊l,k=8πitl,k(τ2)+2πiβl,k2=0.\frac{d}{d(\tau^{2})}\int_{A_{l,k}}\mathfrak{G}_{l,k}=-8\pi{\rm i}\frac{\partial t_{l,k}}{\partial(\tau^{2})}+2\pi{\rm i}\beta_{l,k}^{2}=0.

This proves the claimed partial derivatives with respect to τ2\tau^{2}. ∎

Remark 17.

We see from the computations that our local coordinates ww and ww^{\prime} are chosen for convenience. Had we used other coordinates, the computations would be very difference, but (αl,kiσl,0γl,k)/(τ2)\partial(\alpha_{l,k}-{\rm i}\sigma_{l,0}\gamma_{l,k})/\partial(\tau^{2}) would be invariant, and tl,k/(τ2)\partial t_{l,k}/\partial(\tau^{2}) would be rescaled to keep the conformal type of Σt\Sigma_{t} (to the first order). So the choice of local coordinates has no substantial impact on our construction.

3.3.2. Solving B-period problems

In the following, we make a change of variable τ=exp(1/ξ2)\tau=\exp(-1/\xi^{2}).

Proposition 11.

Assume that the parameters tl,kt_{l,k}, αl,k\alpha_{l,k}, and γl,k\gamma_{l,k} are given by Proposition 10. For ξ\xi sufficiently small and pl,kp_{l,k} and pl,kp^{\prime}_{l,k} in a neighborhood of their central values, there exist unique values of βl,k\beta_{l,k}, depending smoothly on (ξ,p,p)(\xi,p,p^{\prime}) and (βh)h𝖧(\beta_{h})_{h\in\mathsf{H}}, such that the balance equation (18) with 1lL1\leq l\leq L and the yy-component of the B-period problem (23) are solved. Moreover, at ξ=0\xi=0 and βh=βh=θ˙h\beta_{h}=\beta^{\circ}_{h}=\dot{\theta}_{h}, we have βl,k=βl,1=cl\beta_{l,k}=\beta_{l,1}=-c_{l} where clc_{l} is given by (1).

Proof.

By Lemma 8.3 of [CT21],

(Bl,kΦ~2)βl,klntl,k\Big{(}\int_{B_{l,k}}\widetilde{\Phi}_{2}\Big{)}-\beta_{l,k}\ln t_{l,k}

extends holomorphically to t=0t=0 as bounded analytic functions of other parameters. We have seen that tl,kτ2βl,k2/4t_{l,k}\sim\tau^{2}\beta^{2}_{l,k}/4. So

:=ξ22Re(Bl,kΦ~2Bl,1Φ~2)=βl,kβl,1\mathfrak{H}:=-\frac{\xi^{2}}{2}\operatorname{Re}\Big{(}\int_{B_{l,k}}\widetilde{\Phi}_{2}-\int_{B_{l,1}}\widetilde{\Phi}_{2}\Big{)}=\beta_{l,k}-\beta_{l,1}

at ξ=0\xi=0. Therefore, =0\mathfrak{H}=0 is solved at ξ=0\xi=0 by βl,k=βl,1\beta_{l,k}=\beta_{l,1} for all 2knl2\leq k\leq n_{l}, and βl,1=cl\beta_{l,1}=-c_{l} follows as (1) is just a reformulation of (18). The proposition then follows by the Implicit Function Theorem. ∎

Proposition 12.

Assume that the parameters tl,kt_{l,k}, αl,k\alpha_{l,k}, βl,k\beta_{l,k} and γl,k\gamma_{l,k} are given by Propositions 10 and 11. For ξ\xi sufficiently small and pl,kp_{l,k} in a neighborhood of their central values, there exist unique values of pl,kp^{\prime}_{l,k}, depending smoothly on ξ\xi, pp, and (βh)h𝖧(\beta_{h})_{h\in\mathsf{H}}, such that the xx- and zz-components of the B-period problem (23) are solved. Moreover, up to complex scalings on l+1×\mathbb{C}^{\times}_{l+1}, 1lL1\leq l\leq L, we have pl,k=pl,k¯p^{\prime}_{l,k}=\overline{p_{l,k}} at ξ=0\xi=0 for any 1<knl1<k\leq n_{l}.

Proof.

At ξ=0\xi=0, recall that Φ1=dz/z\Phi_{1}=dz/z and Φ3=iσl,0dz/z\Phi_{3}=-{\rm i}\sigma_{l,0}dz/z. So

ReBl,kΦ1ReBl,1Φ1\displaystyle\operatorname{Re}\int_{B_{l,k}}\Phi_{1}-\operatorname{Re}\int_{B_{l,1}}\Phi_{1} =Reln(pl,k/pl,1)Reln(pl,k/pl,1);\displaystyle=\operatorname{Re}\ln(p_{l,k}/p_{l,1})-\operatorname{Re}\ln(p^{\prime}_{l,k}/p^{\prime}_{l,1});
ReBl,kΦ3ReBl,1Φ3\displaystyle\operatorname{Re}\int_{B_{l,k}}\Phi_{3}-\operatorname{Re}\int_{B_{l,1}}\Phi_{3} =σl,0(Imln(pl,k/pl,1)+Imln(pl,k/pl,1)).\displaystyle=\sigma_{l,0}(\operatorname{Im}\ln(p_{l,k}/p_{l,1})+\operatorname{Im}\ln(p^{\prime}_{l,k}/p^{\prime}_{l,1})).

They vanish if and only if ln(pl,k/pl,1)=ln(pl,k/pl,1)¯\ln(p_{l,k}/p_{l,1})=\overline{\ln(p^{\prime}_{l,k}/p^{\prime}_{l,1})}. We normalize the complex scaling on l+1×\mathbb{C}^{\times}_{l+1}, 1lL1\leq l\leq L, by fixing pl,1=pl,1¯p^{\prime}_{l,1}=\overline{p_{l,1}}. Then the B-period problem is solved at ξ=0\xi=0 with pl,k=pl,k¯p^{\prime}_{l,k}=\overline{p_{l,k}}. By the same argument as in [Tra08], the integrals are smooth functions of ξ\xi and other parameters, so the proposition follows by the Implicit Function Theorem. ∎

3.3.3. Balancing conditions

Define

l,k=Res(zΦ~22dz,pl,k)andl,k=Res(zΦ~22dz,pl,k).\mathfrak{R}_{l,k}=\operatorname{Res}\left(\frac{z\widetilde{\Phi}_{2}^{2}}{dz},p_{l,k}\right)\quad\text{and}\quad\mathfrak{R}^{\prime}_{l,k}=\operatorname{Res}\left(\frac{z\widetilde{\Phi}_{2}^{2}}{dz},p^{\prime}_{l,k}\right).

Let the central values pl,k=conjlql,kp^{\circ}_{l,k}=\operatorname{conj}^{l}q_{l,k}, where qq is from a balanced configuration. So the central values pl,k=conjl+1ql,kp^{\prime\circ}_{l,k}=\operatorname{conj}^{l+1}q_{l,k} and

Φ~2={conjψl¯on l× for l odd,ψlon l× for l even.\widetilde{\Phi}^{\circ}_{2}=\begin{cases}\overline{\operatorname{conj}^{*}\psi_{l}}&\text{on $\mathbb{C}^{\times}_{l}$ for $l$ odd,}\\ \psi_{l}&\text{on $\mathbb{C}^{\times}_{l}$ for $l$ even.}\end{cases}

Then we have

l,k¯+l,k=2conjl+1Fl,k\overline{\mathfrak{R}_{l,k}}+\mathfrak{R}^{\prime}_{l,k}=2\operatorname{conj}^{l+1}F_{l,k}

at the central values, where Fl,kF_{l,k} is the force given by (4). Moreover, by Residue Theorem on l×\mathbb{C}^{\times}_{l},

(29) k=1nl1l1,k+k=1nll,k+βl,02βl,2=0.\sum_{k=1}^{n_{l-1}}\mathfrak{R}^{\prime}_{l-1,k}+\sum_{k=1}^{n_{l}}\mathfrak{R}_{l,k}+\beta_{l,0}^{2}-\beta_{l,\infty}^{2}=0.
Proposition 13.

Assume that the parameters tl,kt_{l,k}, αl,k\alpha_{l,k}, and γl,k\gamma_{l,k} are given as analytic functions of τ2\tau^{2} by Proposition 10. Then 𝔉~l,k:=τ2𝔉l,k\widetilde{\mathfrak{F}}^{\prime}_{l,k}:=\tau^{-2}\mathfrak{F}^{\prime}_{l,k} extends analytically to τ=0\tau=0 with the value

{4πiconjl+1Fl,k,2knl,4πiconjl+1(Fl,1+j=1l1k=1njFj,k),k=1.\begin{dcases}4\pi{\rm i}\operatorname{conj}^{l+1}F_{l,k},&2\leq k\leq n_{l},\\ 4\pi{\rm i}\operatorname{conj}^{l+1}\Big{(}F_{l,1}+\sum_{j=1}^{l-1}\sum_{k=1}^{n_{j}}F_{j,k}\Big{)},&k=1.\end{dcases}
Proof.

If f(z)f(z) is an analytic function in zz and f(0)=0f(0)=0, then f(z)/zf(z)/z extends analytically to z=0z=0 with the value df/dzz=0df/dz\mid_{z=0}. We compute at τ=0\tau=0 that

α𝔉l,k=4πiandγ𝔉l,k=4πσl,0.\frac{\partial}{\partial\alpha}\mathfrak{F}^{\prime}_{l,k}=-4\pi{\rm i}\quad\text{and}\quad\frac{\partial}{\partial\gamma}\mathfrak{F}^{\prime}_{l,k}=4\pi\sigma_{l,0}.

Then

dd(τ2)𝔉l,k=4πiαl,k(τ2)+4πσl,0γl,k(τ2)+2πil,k.\frac{d}{d(\tau^{2})}\mathfrak{F}^{\prime}_{l,k}=-4\pi{\rm i}\frac{\partial\alpha_{l,k}}{\partial(\tau^{2})}+4\pi\sigma_{l,0}\frac{\partial\gamma_{l,k}}{\partial(\tau^{2})}+2\pi{\rm i}\mathfrak{R}^{\prime}_{l,k}.

For 2knl2\leq k\leq n_{l}, by (28), 𝔉~l,k:=τ2𝔉l,k\widetilde{\mathfrak{F}}^{\prime}_{l,k}:=\tau^{-2}\mathfrak{F}^{\prime}_{l,k} extends to τ=0\tau=0 with the value

dd(τ2)𝔉l,k=2πi(l,k¯+l,k)=4πiconjl+1Fl,k.\frac{d}{d(\tau^{2})}\mathfrak{F}^{\prime}_{l,k}=2\pi{\rm i}(\overline{\mathfrak{R}_{l,k}}+\mathfrak{R}^{\prime}_{l,k})=4\pi{\rm i}\operatorname{conj}^{l+1}F_{l,k}.

As for k=1k=1 and l<Ll<L, we compute at τ=0\tau=0

k=1nld𝔉l,kd(τ2)+k=1nl1conj(d𝔉l1,kd(τ2))\displaystyle\sum_{k=1}^{n_{l}}\frac{d\mathfrak{F}^{\prime}_{l,k}}{d(\tau^{2})}+\sum_{k=1}^{n_{l-1}}\operatorname{conj}\Big{(}\frac{d\mathfrak{F}^{\prime}_{l-1,k}}{d(\tau^{2})}\Big{)}
=\displaystyle= 4πiτ2(k=1nlαl,kk=1nl1αl1,k)\displaystyle-4\pi{\rm i}\frac{\partial}{\partial\tau^{2}}\bigg{(}\sum_{k=1}^{n_{l}}\alpha_{l,k}-\sum_{k=1}^{n_{l-1}}\alpha_{l-1,k}\bigg{)}
+4πσl,0τ2(k=1nlγl,kk=1nl1γl1,k)\displaystyle+4\pi\sigma_{l,0}\frac{\partial}{\partial\tau^{2}}\bigg{(}\sum_{k=1}^{n_{l}}\gamma_{l,k}-\sum_{k=1}^{n_{l-1}}\gamma_{l-1,k}\bigg{)} (because σl1,0=σl,0\sigma_{l-1,0}=-\sigma_{l,0})
+2πi(k=1nll,kk=1nl1l1,k¯)\displaystyle+2\pi{\rm i}\bigg{(}\sum_{k=1}^{n_{l}}\mathfrak{R}^{\prime}_{l,k}-\sum_{k=1}^{n_{l-1}}\overline{\mathfrak{R}^{\prime}_{l-1,k}}\bigg{)}
=\displaystyle= 4πiτ2(αl,0+αl,)4πσl,0τ2(γl,0+γl,)\displaystyle 4\pi{\rm i}\frac{\partial}{\partial\tau^{2}}(\alpha_{l,0}+\alpha_{l,\infty})-4\pi\sigma_{l,0}\frac{\partial}{\partial\tau^{2}}(\gamma_{l,0}+\gamma_{l,\infty}) (by (17) and (19))
+2πi(k=1nll,k+k=1nll,k¯+βl,02βl,2)\displaystyle+2\pi{\rm i}\bigg{(}\sum_{k=1}^{n_{l}}\mathfrak{R}^{\prime}_{l,k}+\sum_{k=1}^{n_{l}}\overline{\mathfrak{R}_{l,k}}+\beta_{l,0}^{2}-\beta_{l,\infty}^{2}\bigg{)} (by (29))
=\displaystyle= 2πi(βl,2βl,02+k=1nl(l,k¯+l,k)+βl,02βl,2)\displaystyle 2\pi{\rm i}\Big{(}\beta_{l,\infty}^{2}-\beta_{l,0}^{2}+\sum_{k=1}^{n_{l}}(\overline{\mathfrak{R}_{l,k}}+\mathfrak{R}^{\prime}_{l,k})+\beta_{l,0}^{2}-\beta_{l,\infty}^{2}\Big{)} (by (21))
=\displaystyle= 4πik=1nlconjl+1Fl,k.\displaystyle 4\pi{\rm i}\sum_{k=1}^{n_{l}}\operatorname{conj}^{l+1}F_{l,k}.

Then

k=1nld𝔉l,kd(τ2)=\displaystyle\sum_{k=1}^{n_{l}}\frac{d\mathfrak{F}^{\prime}_{l,k}}{d(\tau^{2})}= d𝔉l,1d(τ2)+4πiconjl+1k=2nlFl,k\displaystyle\frac{d\mathfrak{F}^{\prime}_{l,1}}{d(\tau^{2})}+4\pi{\rm i}\operatorname{conj}^{l+1}\sum_{k=2}^{n_{l}}F_{l,k}
=\displaystyle= (conj)lm=1l(conj)m(k=1nmd𝔉m,kd(τ2)+k=1nm1conj(d𝔉m1,kd(τ2)))\displaystyle(-\operatorname{conj})^{l}\sum_{m=1}^{l}(-\operatorname{conj})^{m}\bigg{(}\sum_{k=1}^{n_{m}}\frac{d\mathfrak{F}^{\prime}_{m,k}}{d(\tau^{2})}+\sum_{k=1}^{n_{m-1}}\operatorname{conj}\Big{(}\frac{d\mathfrak{F}^{\prime}_{m-1,k}}{d(\tau^{2})}\Big{)}\bigg{)}
=\displaystyle= (conj)lm=1l(conj)m(4πik=1nmconjm+1Fm,k)\displaystyle(-\operatorname{conj})^{l}\sum_{m=1}^{l}(-\operatorname{conj})^{m}\Big{(}4\pi{\rm i}\sum_{k=1}^{n_{m}}\operatorname{conj}^{m+1}F_{m,k}\Big{)}
=\displaystyle= 4πiconjl+1m=1lk=1nmFm,k,\displaystyle 4\pi{\rm i}\operatorname{conj}^{l+1}\sum_{m=1}^{l}\sum_{k=1}^{n_{m}}F_{m,k},

so 𝔉~l,1:=τ2𝔉l,1\widetilde{\mathfrak{F}}^{\prime}_{l,1}:=\tau^{-2}\mathfrak{F}^{\prime}_{l,1} extends to τ=0\tau=0 with the value

d𝔉l,1d(τ2)=4πiconjl+1(Fl,1+m=1l1k=1nmFm,k).\frac{d\mathfrak{F}^{\prime}_{l,1}}{d(\tau^{2})}=4\pi{\rm i}\operatorname{conj}^{l+1}\Big{(}F_{l,1}+\sum_{m=1}^{l-1}\sum_{k=1}^{n_{m}}F_{m,k}\Big{)}.

Therefore, if (q,θ˙)(q,\dot{\theta}) is balanced, 𝔉~=0\widetilde{\mathfrak{F}}^{\prime}=0 is solved at τ=0\tau=0. Recall that we normalize the complex scaling on 1×\mathbb{C}^{\times}_{1} by fixing p1,1p_{1,1}. If (q,θ˙)(q,\dot{\theta}) is rigid, because Θ2=Fl,k=0\Theta_{2}=\sum F_{l,k}=0 independent of pp, the partial derivative of (𝔉~)(l,k)(L,1)(\widetilde{\mathfrak{F}}^{\prime})_{(l,k)\neq(L,1)} with respect to (pl,k)(l,k)(1,1)(p_{l,k})_{(l,k)\neq(1,1)} is an isomorphism from N1\mathbb{C}^{N-1} to N1\mathbb{C}^{N-1}. The following proposition then follows by the Implicit Function Theorem.

Proposition 14.

Assume that the parameters tl,kt_{l,k}, αl,k\alpha_{l,k}, βl,k\beta_{l,k}, γl,k\gamma_{l,k}, pl,kp^{\prime}_{l,k} are given by Propositions 10, 11, and 12. Assume further that the central values ql,k=conjlpl,kq_{l,k}=\operatorname{conj}^{l}p^{\circ}_{l,k} and θ˙h=βh\dot{\theta}_{h}=\beta^{\circ}_{h} form a balanced and rigid configuration (q,θ˙)(q,\dot{\theta}). Then for (τ,β)(\tau,\beta) in a neighborhood of (0,θ˙)(0,\dot{\theta}) that solves (20) and (22), there exists values for pl,kp_{l,k}, unique up to a complex scaling, depending smoothly on τ\tau and (βh)h𝖧(\beta_{h})_{h\in\mathsf{H}}, such that pl,k(0,θ˙)=pl,kp_{l,k}(0,\dot{\theta})=p^{\circ}_{l,k} and the conformality condition (26) is solved.

3.4. Embeddedness

It remains to prove that

Proposition 15.

The minimal immersion given by the Weierstrass parameterization is regular and embedded.

Proof.

The immersion is regular if |Φ1|2+|Φ2|2+|Φ3|2>0|\Phi_{1}|^{2}+|\Phi_{2}|^{2}+|\Phi_{3}|^{2}>0. This is easily verified on UδU_{\delta}. On the necks and the ends, the regularity follows if we prove that Φ~2\widetilde{\Phi}_{2} has no zeros outside UδU_{\delta}. At τ=0\tau=0, Φ~2\widetilde{\Phi}_{2} has nl+nl1+2n_{l}+n_{l-1}+2 poles on ^l\hat{\mathbb{C}}_{l}, hence nl+nl1n_{l}+n_{l-1} zeros. By taking δ\delta sufficiently small, we may assume that all these zeros lie in Ul,δU_{l,\delta}. By continuity, Φ~2\widetilde{\Phi}_{2} has nl+nl2n_{l}+n_{l-2} zeros in Ul,δU_{l,\delta} also for τ\tau sufficiently small. But for τ0\tau\neq 0, Φ~2\widetilde{\Phi}_{2} is meromorphic on a Riemann surface Στ\Sigma_{\tau} of genus g=NLg=N-L and has 2L+22L+2 simple poles, hence has 2(NL)2+2L+2=2N2(N-L)-2+2L+2=2N zeros. So Φ~2\widetilde{\Phi}_{2} has no further zeros, in Σt\Sigma_{t}, in particular not outside UδU_{\delta}.

We now prove that the immersion

zRez(Φ1,Φ~2,Φ3)z\mapsto\operatorname{Re}\int^{z}(\Phi_{1},\widetilde{\Phi}_{2},\Phi_{3})

is an embedding, and the limit positions of the necks are as prescribed.

On Ul,δU_{l,\delta}, the Gauss map G=(Φ1+iΦ2)/Φ3G=-(\Phi_{1}+{\rm i}\Phi_{2})/\Phi_{3} converges to iσl,0{\rm i}\sigma_{l,0}, so the immersion is locally a graph over the xzxz-plane. Fix an orientation σ1,0=1\sigma_{1,0}=-1, then up to translations, we have

limτ0(RezΦ1+iRezΦ3)=conjl(lnz)+2mπi\lim_{\tau\to 0}\Big{(}\operatorname{Re}\int^{z}\Phi_{1}+{\rm i}\operatorname{Re}\int^{z}\Phi_{3}\Big{)}=\operatorname{conj}^{l}(\ln z)+2m\pi{\rm i}

where mm depends on the integral path, and

limτ0RezΦ~2=Rez(conj)lψl=:Ψl(conjlz)\lim_{\tau\to 0}\operatorname{Re}\int^{z}\widetilde{\Phi}_{2}=\operatorname{Re}\int^{z}(\operatorname{conj}^{*})^{l}\psi_{l}=:\Psi_{l}(\operatorname{conj}^{l}z)

which is well defined for zUl,δz\in U_{l,\delta} because the residues of ψl\psi_{l} are all real.

With a change of variable zlnzz\mapsto\ln z, we see that the immersion restricted to Ul,δU_{l,\delta} converges to a periodic graph over the xzxz-planes, defined within bounded xx-coordinate and away from the points lnql,k+2mπi\ln q_{l,k}+2m\pi{\rm i}, and the period is 2πi2\pi{\rm i}. Here, again, we identified the xzxz-plane with the complex plane.

This graph must be included in a slab parallel to the xzxz-plane with bounded thickness. We have seen from the integration along BkB_{k} that the distance between adjacent slabs is of the order 𝒪(lnτ)\mathcal{O}(\ln\tau). So the slabs are disjoint for τ\tau sufficiently small.

As for the necks and ends, note that there exists Y>0Y>0 such that Ψl1([Y,Y])\Psi_{l}^{-1}([-Y,Y]) is bounded by nl+nl1+2n_{l}+n_{l-1}+2 convex curves. After the change of variable zlnzz\mapsto\ln z, all but two of these curves remain convex; those around 0 and \infty become periodic infinite curves. If YY is chosen sufficiently large, there exists X>0X>0 independent of ll such that the curves |z|=exp(±X)|z|=\exp(\pm X) are included in Ψl1([Y,Y])\Psi_{l}^{-1}([-Y,Y]) for every 1lL+11\leq l\leq L+1. After the change of variable zlnzz\mapsto\ln z, these curves become curves with Rez=±X\operatorname{Re}z=\pm X.

Hence for τ\tau sufficiently small, we may find Yl+Y^{+}_{l} and YlY^{-}_{l}, with Yl<Yl+<Yl+1Y^{-}_{l}<Y^{+}_{l}<Y^{-}_{l+1}, and X>0X>0, such that

  • The immersion with Yl<y<Yl+Y^{-}_{l}<y<Y^{+}_{l} and X<x<X-X<x<X is a graph bounded by nl+nl1n_{l}+n_{l-1} planar convex curves parallel to the xzxz-plane, and two periodic planar infinite curves parallel to the yzyz-plane.

  • The immersion with Yl+<y<Yl+1Y^{+}_{l}<y<Y^{-}_{l+1} and X<x<X-X<x<X consists of annuli, each bounded by two planar convex curves parallel to the xzxz-plane. These annuli are disjoint and, by a Theorem of Schiffman [Shi56], all embedded.

  • The immersion with |x|>X|x|>X are ends, i.e. graphs over vertical half-planes, extending in the direction (1,θ˙l,0)(-1,-\dot{\theta}_{l,0}) and (+1,θ˙l,)(+1,-\dot{\theta}_{l,\infty}), 1lL+11\leq l\leq L+1. If the inequality (5) is satisfied, these graphs are disjoint.

This finishes the proof of embeddedness. ∎

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