Bounded Diameter Under Mean Curvature Flow
Abstract
We prove that for the mean curvature flow of closed embedded hypersurfaces, the intrinsic diameter stays uniformly bounded as the flow approaches the first singular time, provided all singularities are of neck or conical type. In particular, assuming Ilmanen’s multiplicity one conjecture and no cylinder conjecture, we conclude that in the two-dimensional case the diameter always stays bounded. We also obtain sharp bound for the curvature. The key ingredients for our proof are the Lojasiewicz inequalities by Colding-Minicozzi and Chodosh-Schulze, and the solution of the mean-convex neighborhood conjecture by Choi, Haslhofer, Hershkovits and White. Our results improve the prior results by Gianniotis-Haslhofer, where diameter and curvature control has been obtained under the more restrictive assumption that the flow is globally two-convex.
1 Introduction
For a family of closed embedded hypersurfaces in evolving under mean curvature flow, the first singular time is characterized by
(1.1) |
where denotes the norm of second fundamental form.
The central topic for mean curvature flow is to capture the geometric information of singularities. One naturally wonders if one can control the geometry of surfaces evolving under mean curvature flow near the singular time. In particular, we have the following well-known conjecture:
Conjecture 1.1 (bounded diameter conjecture).
For the mean curvature flow of closed embedded hypersurfaces , the intrinsic diameter stays uniformly bounded as the flow approaches to the first singular time , i.e.
where is the geodesic distance on the hypersurface .
We note that while the extrinsic diameter obviously stays bounded, controlling the intrinsic diameter is much more delicate. For example, one has to exclude the existence of fractal-like necks.
The bounded diameter conjecture is also related to the question of establishing sharp integral curvature bounds. In fact, Topping [Top08] proved that
(1.2) |
Recently, Gianniotis-Haslhofer [GH17] proved the bounded diameter conjecture under the assumption that the flow is globally two-convex, i.e. when the sum of any two principal curvatures of each hypersurface is positive.
Theorem 1.2 (Gianniotis-Haslhofer, [GH17, Thm 1.1, Thm 1.2]).
If is a mean curvature flow of two-convex closed embedded hypersurfaces, then
(1.3) |
and moreover,
(1.4) |
where only depends on certain geometric parameters of the initial hypersurface .
Their proof uses the Lojasiewicz inequality from Colding-Minicozzi [CM15] and the canonical neighborhood theorem from Haslhofer-Kleiner [HK17]. In particular, their results improved the earlier - curvature bound from Head [Hea13] and Cheeger-Haslhofer-Naber [CHN13]. In fact, the diameter bound and the curvature bound without depend on the fine structure of singularities. Roughly speaking, the idea is that by the canonical neighborhood theorem, the high curvature regions look like necks or caps, and the Lojasiewicz inequality controls the tilting of the necks. The curvature bound can fail if one removes the two-convexity assumption. For instance, it fails if is a thin rotationally symmetric torus.
1.1 Main results
In this paper, we generalize the diameter and curvature bounds from Gianniotis-Haslhofer [GH17]. Instead of the global two-convexity assumption, we only impose an infinitesimal assumption on the structure of singularities. To describe this, let us first recall the notion of a tangent flow. For in and , we denote by the flow which is obtained by shifting to space-time origin and parabolically dilating by . Now, given any sequence , by Brakke’s compactness theorem [Ilm94, Thm 7.1], one can always pass to a subsequential limit of . Any such limit is called a tangent flow at . From Huisken’s monontonicity formula [Hui90, Thm 3.1], all tangent flows are self-similarly shrinking ancient flows.
If the tangent flow is compact, one can verify the above Conjecture 1.1 easily from the uniqueness result of compact tangent flow of Schulze [Sch14]. In the non-compact tangent flow case, one typically sees cylindrical singularities or conical singularities. Because the curvature bound can fail for singularities, where , as we discussed in the end of previous section, we assume all cylindrical singularities are of neck type, i.e. . The precise definition of neck and conical singularities is as follows:
Definition 1.3 (singularities of neck or conical type).
We say that a singularity of mean curvature flow at a space-time point is of
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•
neck type, if some tangent flow at is a one -factor cylindrical flow (up to a rotation) with multiplicity one.
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•
conical type, if some tangent flow at is with multiplicity one, where is an asymptotically conical shrinker.
We recall that an asymptotically conical shrinker is a smooth hypersurface that satisfies
and
Here the convergence is in with multiplicity one, and is a cone over a closed hypersurface . Now, we state our main result as follows:
Theorem 1.4 (diameter bound).
Let be a family of closed embedded hypersurfaces in evolving under mean curvature flow with first singular time . If every singularity at time is of neck type or conical type (see Definition 1.3), then
We also have the following sharp curvature bound.
Theorem 1.5 (curvature bound).
Under the same assumptions as in Theorem 1.4, we have
Theorem 1.4 and Theorem 1.5 improve the main results of Gianniotis-Haslhofer [GH17, Thm 1.1, Thm 1.2] by removing the global two-convexity assumption in a favor of a much milder infinitesimal assumption on the structure of singularities.
Our conclusion is most striking for , i.e. in the classical case of -dimension surfaces in .
In fact, we obtain the bounded diameter conjecture in full generality assuming Ilmanen’s multiplicity one conjecture and no cylinder conjecture. Let us recall these conjectures:
Conjecture 1.6 (Ilmanen, [Ilm03, 2. multiplicity one conjecture.]).
Let be a smooth embedded compact initial surface in with mean curvature flow . Then a higher multiplicity plane cannot occur as a blowup limit of at the first singular time.
Conjecture 1.7 (Ilmanen, [Ilm03, 12. No cylinder conjecture.]).
Let be an embedded shrinking soliton in , and suppose that is not a round cylinder. Then, cannot have an end asymptotic to a cylinder.
This reduction of assumptions is based on the following facts in the case where . First, Ilmanen [Ilm95] proved that for embedded mean curvature flow, every tangent flow is smoothly embedded. Then, Wang [Wan14] proved that every non-compact tangent flow must have cylindrical and conical ends. Also, a more than one -factor cylindrical flow is obviously excluded, so the above two conjectures imply that for , we can only see singularities of neck type or conical type, or singularities whose blowing-up is compact tangent flow, Hence, we obtain the general conclusion for :
Corollary 1.8 (diameter and curvature bounds for .).
Let be a family of closed embedded surfaces in evolving under mean curvature flow with first singular time , if we assume Ilmanen’s multiplicity one and no cylinder conjecture, then we have
and
1.2 Ideas and key ingredients
The main difficulty is to control the geodesic length in regions which contain singularities and have high curvature because diameter can be uniformly controlled in the regions which have bounded geometry. To overcome the difficulty, we need to use the infinitesimal assumption on the structure of singularities to decompose the flow into a low curvature part and a part that can be well approximated in terms of certain standard geometric models. Since we only see singularities of cylindrical type and conical type, we can actually decompose the flow into the following more precise three parts (see Theorem 5.1):
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•
low curvature part,
-
•
mean convex part,
-
•
conical part.
For obtaining this decomposition, the following two ingredients are important: the existence of mean convex canonical neighborhoods and a precise description of neighborhoods of conical singularities.
First, based on the solutions to mean convex canonical neighborhood conjecture proved by Choi, Haslhofer, Hershkovits and White (see [CHH18] and [CHHW19]), we obtain the existence of mean convex canonical neighborhoods (see Theorem 3.1). For instance, when , we prove this by contradiction using the classification of ancient low entropy flows (see [CHH18, Thm 1.2]).
Then, by adapting the methods from Chodosh and Schulze’s work of proving uniqueness of conical tangent flow in [CS19], we obtain a precise description of neighborhoods of conical singularities (see Proposition 4.2). More precisely, we use their uniqueness result and obtain the estimates in a certain region of space-time with conical singularity as tip. Then, we need to extend the estimates into some parabolic ball with conical singularity as center. The strategies are applying pseudolocality and Ecker-Huisken’s curvature estimate to the renormalized flow and then rescale the estimates back.
Next, using the previous decomposition, we reduce to estimating diameter in tubes, i.e. regions entirely covered by necks (see Proposition 6.5). This is related to [GH17, Prop 3.2] but one difference here is that we need to use Proposition 4.2 to control the length of geodesics near conical singularities.
For dealing with the estimation in tubes, we need the following two ingredients: backwards stability (Proposition 7.1) and small axis tilt (Proposition 7.2). Since bowl soliton and cylindrical flow are all the possible models in mean convex canonical neighborhoods (Theorem 3.1), we only need to prove backwards stability for these two models. On the other hand, motivated by the Lojasiewicz inequality and uniqueness argument of Colding and Minicozzi (see [CM15]), we obtain the small axis tilt.
Then, using backwards stability and small axis tilt, we show that in the neck region, the flow is close to tube flow with small tilt during a uniform period of time before the singular time . Thus, we obtain the uniform control of the diameters in tubes, which by the above reductions yields a global diameter bound. This completes the sketch of the proof of Theorem 1.4.
Finally, for proving Theorem 1.5, we estimate the curvature integral in all the three parts obtained by Theorem 5.1. We show that mean convex part is the union of controlled number of tubes and caps, and Theorem 1.4 implies the curvature bound in the tubes. The curvature bound in low curvature part, cap part, and conical part can be easily obtained. This completes the sketch of the proof of Theorem 1.5.
1.3 Organization of the paper
We organized the paper as follows:
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In Section 2, we introduce some general definitions and summarize necessary preliminaries.
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Acknowledgements
The author acknowledges his supervisor Robert Haslhofer for his patient guidance and invaluable support in bringing this paper into fruition over the last year.
2 Preliminaries
In this section, we collect some general definitions and facts that will be used throughout the paper.
Definition 2.1 (Brakke flow, [Ilm94, Def 6.2]).
An -dimensional integral Brakke flow is a one parameter family of Radon measures on such that
-
(i)
For almost every , , where is an integral dimensional varifold in , such that for every vector field ,
holds for some vector valued function .
-
(ii)
For every nonnegative function , where , we have
-
(iii)
For almost every , there are a -valued function and a -dimensional rectifiable set , such that
Definition 2.2 (convergence of Brakke flow, [Ilm94]).
A sequence of Brakke flows converges to , which is denoted by , if the following two properties hold.
-
(i)
For all and , we have
-
(ii)
For almost every , there is a subsequence depending on , such that
as varifolds.
Definition 2.3 (entropy, [CM12]).
Let be dimensional integral rectifiable Radon measure. The entropy of is given by
The entropy of Brakke flow is given by
For mean curvature flow, we have following Huisken’s monontonicity formula:
Theorem 2.4 (Huisken’s monontonicity formula, [Hui90, Thm 3.1]).
Let in be a family of closed smoothly embedded hypersurfaces evolving under mean curvature flow, be a space-time point, and
Then,
(2.1) |
If one replaces the equality in (2.1) by an inequality, then it holds for Brakke flow.
As a consequence of Huisken’s monotonicity formula, the Gaussian density can be defined as follows:
Definition 2.5 (Gaussian density).
For Brakke flow and a space-time point , the Gaussian density of at is given by
Now, we state Brakke’s compactness theorem (formulated in terms of entropy):
Theorem 2.6 (Brakke’s compactness theorem, [Ilm94, Thm 7.1]).
For a family of integral Brakke flows , if the entropy of is uniformly bounded, then (in Brakke flow’s convergence) and is still an integral Brakke flow.
The next two definitions are useful in our proof of diameter bound of mean curvature flow.
Definition 2.7 (-close).
Let be a smooth mean curvature flow and be a space-time point. is -close to some mean curvature flow at , if is the graph of function over , and
holds for all and for all .
Definition 2.8 (regularity scale).
We define the regularity scale of mean curvature flow at as the supremum of , such that is a smooth graph for all and such that for all , where and , we have
(2.2) |
The important result related to regularity scale is White’s local regularity theorem:
Theorem 2.9 (local regularity theorem, [Whi05]).
There are universal constants and with the following significance: Let be a smooth proper mean curvature flow in , . If the Gaussian density , then there is a , such that
holds for every and every .
As a consequence of local regularity theorem, if a sequence of Brakke flows converges in the sense of Brakke flows and the limit is smooth, then the convergence is smooth.
3 Mean convex canonical neighborhoods
In this section, we discuss the structure of the flow near neck singularities. By the solution of mean convex neighborhood conjecture in [CHH18, Thm 1.6] and [CHHW19, Thm1.15], every neck singularity has a space-time neighborhood where the flow moves in one direction. More precisely, we have the following result.
Theorem 3.1 (mean convex canonical neighborhoods, c.f. [CHH18, CHHW19]).
Let be a smooth mean curvature flow with first singular time . Assume some tangent flow at is a multiplicity one cylindrical flow with one -factor. Then, for every , there is a , such that any is -close (see Definition 2.7) to either a one -factor cylinder shrinker or a bowl soliton. In particular, is mean convex in the above neighborhood.
We recall that the bowl soliton is the unique (up to rigid motion and scaling) translating solution of the mean curvature flow that is rotationally symmetric and strictly convex, see [AW94, CSS07, Has15].
For , Theorem 3.1 has been obtained in [CHHW19, Cor 1.18] as a consequence of classification of ancient asymptotically cylindrical flows. In a similar vein, we shall see that the statement for ultimately follows from the classification of ancient low entropy flows in [CHH18, Thm 1.2]. Since neither the statement about canonical neighborhoods nor its proof appeared in [CHH18], let us give a detailed proof here. To this end, we first recall the classification of ancient low entropy flows.
Definition 3.2 (ancient low entropy flow, [CHH18, Def 1.1]).
An ancient low entropy flow is an ancient, unit regular, cyclic integral Brakke flow in with .
Here, a Brakke flow is called ancient if it is defined on some interval starting from , and unit regular [Whi05] if every space-time point with density is a regular point. Being cyclic means, loosely speaking, that the flow has an inside and an outside, see [Whi09] for the precise definition.
Theorem 3.3 (classification of ancient low entropy flow, [CHH18, Thm 1.2]).
Every ancient low entropy flow in is one of the following: (i) static plane, (ii) round shrinking sphere, (iii) ancient oval, (iv) one -factor cylinder, (v) bowl soliton.
Here, we recall that an ancient oval is ancient noncollapsed mean curvature flow of embedded 2-spheres that is not selfsimilar, see [Whi03, HH16] for existence and [ADS18] for uniqueness.
By the discussion above, our task is to establish the existence of canonical neighborhoods in the case .
Proof of Theorem 3.1.
Suppose towards a contradiction, there exists , such that for all , we can find in that is neither -close to a one -factor cylinder nor to a bowl soliton.
Let be the regularity scale of (see Definition 2.8). Because is singular, we have that converges to . Let be the flow which is obtained from by shifting to the space-time origin and parabolically rescaling by . By the uniform boundedness of the entropy of and by Brakke’s compactness theorem in [Ilm94, Thm 7.1], we can pass to a subsequential limit , which is an integral Brakke flow.
Claim. is an ancient low entropy flow.
Proof of claim.
By the above analysis and by [Whi05] [Whi09, Thm 4.2], we know that is an integral, unit regular and cyclic Brakke flow.
By the definition of entropy of , and since the rescaled flows converges to , for all , we can find and , such that
On the other hand, because is cylindrical singularity, using the upper-semicontinuity of Gaussian density and Huisken’s monontoncity formula [Hui90, Thm 3.1], we know there is some , such that
holds for and .
By Huisken’s monotonicity formula and the arbitrariness of , we obtain
This implies that is an ancient low entropy flow, and thus proves the claim. ∎
Hence, is from one of the five cases in the classification of Theorem 3.3. We will show that all cases yield a contradiction.
(i) If is a static plane, by the local regularity theorem, we obtain that does not converge to , which is a contradiction.
(ii) and (iii). If is a round shrinking sphere or an ancient oval, by the local regularity theorem, for large enough, can be written as a graph of function over with norm less than . This implies that for any given interval , is convex in for large enough if we choose small. Hence, becomes convex after some time close to , so Huisken’s convergence theorem [Hui84] implies that becomes extinct as a round point. This contradicts the assumption that has cylindrical singularity at .
(iv) and (v). Suppose is a one -factor cylinder or a bowl soliton. First note that on the cylinder or bowl soliton, the regularity scale and the inverse mean curvature scale are comparable. Namely, there is a constant , such that,
(3.1) |
holds for all . Recall that was defined by rescaling by , where . Let , where we now rescale the flow by . By the local regularity theorem, converges to smoothly. By this smooth convergence and the inequalities in (3.1), we get that
(3.2) |
holds for large enough. Therefore, we know that the two rescalings for and only differ by a controlled factor. This implies that also converges to a cylinder or a bowl soliton smoothly.
Correspondingly, we know that is -close to a one - factor cylindrical flow or a bowl soliton for large enough. This contradicts our assumption that is neither -close to a one -factor cylinder nor to a bowl soliton.
By the above contradictions, we have completed the proof of the theorem.
∎
4 Neighborhoods of conical singularities
In this section, we discuss the structure of the flow near conical singularities. In [CS19], Chodosh-Schulze proved that asymptotically conical tangent flows are unique and conical singularities are isolated.
Theorem 4.1 (uniqueness of asymptotically conical tangent flows, [CS19, Thm 1.1]).
Let be a mean curvature flow, and suppose that some tangent flow at is with multiplicity one, where is an asymptotically conical shrinker. Then, the tangent flow at is unique. Moreover, there exists , such that the flow is smooth in , and has a conical singularity at smoothly modeled on the asymptotic cone of .
Here, we recall that an asymptotically conical shrinker is a smooth hypersurface which satisfies
and
in with multiplicity one, where is a cone over a closed hypersurface .
For our purpose, we need the following more precise description of a neighborhood of a conical singularity:
Proposition 4.2.
Let be a smooth mean curvature flow, and suppose that some tangent flow at is with multiplicity one, where is an asymptotically conical shrinker. Then, for any and , we can find , such that for , is a smooth graph of some function over with
(4.1) |
For the proof, similarly as in Chodosh-Schulze [CS19], we will combine their uniqueness result (Theorem 4.1) with the pseudolocality theorem, which we now recall:
Theorem 4.3 ([INS19, Theorem 1.5], [CY07, Theorem 1.4]).
Given , there is and , such that if a mean curvature flow satisfies that is a Lipschitz graph over some region of the plane with Lipschitz constant smaller than and , then intersects and remains a Lipschitz graph within over some region of the plane for all time .
As a corollary, we have the following pseudolocality for the renormalized flow , where and .
Corollary 4.4 (pseudolocality for renormalized flow).
Given , there is and , such that if the renormalized mean curvature flow satisfies that is a Lipschitz graph over the plane with Lipschitz constant less than and , then intersects and remains a Lipschitz graph within over the plane for all .
Proof of Proposition 4.2.
Let and be fixed. For ease of notation, we suppose that is defined on with the only conical singularity at . Now, we consider the renormalized flow . By Theorem 4.1 (uniqueness of conical tangent flow), converges to conical shrinker smoothly. Hence, for the given , we can find monotone functions , and as , such that is a graph of some function over with
(4.2) |
provided that is large enough.
Rescaling this back to the original flow, we see that
is a graph of some function over for small enough. Moreover, for the given and , we can find some , where is large enough, such that
(4.3) |
holds for all .
Therefore, we have obtained the desired estimates (4.1) in the parabolic region .
Next, we need to extend the estimates (4.1) from to some parabolic ball with center at . Fo the given and from above, let be a small constant to be fixed later. Then, and will be fixed according to Corollary 4.4 (pseudolality for renormalized flow). Because is an asymptotically conical shrinker, we can find such that for , can be written as graph over with norm less than . Since converges to smoothly, for any , can be written as graphs over -size balls on tangent planes of with norm less than , provided that is large enough.
By Corollary 4.4 (pseudolality for renormalized flow), we see that for all , can be written as pieces of Lipschitz graphs over size balls on tangent planes of .
By Ecker-Huisken’s curvature estimates for graphical flow in [EH91, Thm 3.1, Thm 3.4] (renormalized version), we see that satisfies
(4.4) |
for all and . Here, is a small constant, and is a constant depending on and the datum at time . This implies that is a graph of some function over with
(4.5) |
for .
Now, we rescale this back to the original flow. Then, can be written as graph of some function over .
Note that and , we see that
(4.6) |
holds for .
Now, we choose small enough, such that
(4.7) |
Let . Noticing that is arbitrary and combing this with (4.6), (4.7) and (4.3), we obtain the estimation (4.1) in . This completes the proof of the theorem.
∎
5 Decomposition of the flow
The goal of this section is to decompose the flow into three parts: low curvature part, mean convex part and conical part.
Suppose that is a compact domain in . Let be a mean curvature flow of closed embedded hypersurfaces in with first singular time . Denote by the singular set at time . Assume that for each , some tangent flow at is a one -factor cylindrical or an asymptotically conical shrinker with multiplicity one.
Theorem 5.1 (decomposition of flow).
Under the above assumptions, for every , there exist constants , and a decomposition of the domain
(5.1) |
such that the following statements hold:
-
(i)
is the union of finitely many balls,
(5.2) where for , such that
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(a)
For , the flow is mean convex.
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(b)
Any is -close (see Definition 2.7) to either a round shrinking cylinder with one -factor or a translating bowl soliton.
-
(a)
-
(ii)
is the disjoint union of finitely many balls
(5.3) such that for all and , can be written as graph over with norm less than , where is an asymptotically conical shrinker.
-
(iii)
For and every or , the regularity scale (see Definition 2.8) at satisfies
(5.4)
Proof.
By the local regularity theorem (or Theorem 2.9), we know that the set of all regular space-time points is open. This implies that the singular set at first singular time is closed and bounded, hence it is compact.
By the isolated property of conical singularities from Theorem 4.1, we know there are only finitely many conical singularities at time . For each , we denote by the tangent flow at the conical singularity . Now, according to Theorem 4.1, we can find , such that are disjoint, and for , are smooth graphs over with norm less than .
Hence, is still compact and all remaining singularities are one -factor cylindrical. Now, by Theorem 3.1, for each , we can find , such that the flow is mean convex and any is -close to either a cylindrical shrinker or a bowl soliton. By compactness of , we can find finitely many cylindrical singularities and corresponding to for ,
such that the above properties in statement 2 hold and
.
Now, we choose and take
and
They satisfy the requirements in statement 1 and statement 2.
Let . Note that and are compact sets. By the local regularity theorem, we know the regularity scale is positive over their union. Combining this with the fact that regularity scale is -Lipschitz, we can find some , such that for
and every or , we have
(5.5) |
This completes the proof. ∎
6 Reduction to the neck region
In this section, based on our decomposition from Section 5, we will reduce to estimating the diameter in neck regions.
As in the Section 5, let be a mean curvature flow of closed embedded hypersurfaces in satisfying the assumptions of Theorem 1.4. Let be a large ball that contains . By Theorem 5.1, for every , we can find constants and a decomposition
into a mean convex part , a conical part , and a low curvature part .
First, we reduce to controlling the diameter in . To this end, for any , we consider
(6.1) |
where denotes the regularity scale (see Definition 2.8).
From Theorem 5.1, we know the geodesic in the above definition of is contained in the region . The next proposition reduces to controlling the diameter in .
Proposition 6.1.
There exists a constant , such that
(6.2) |
Proof.
Let be a minimizing geodesic parametrized by arclength. We choose a maximal collection , such that and for . Let to a geodesic ball with center and radius . These balls are disjoint. Because the regularity scale is bounded below by at , we have a uniform bound on the second fundamental form within balls of definite size with center . By Gauss-Codazzi equation, the sectional curvatures are uniformly bounded within these balls of definite size. According to volume comparison, we get a uniform lower bound for the volume of , i.e
Denoting by the area of initial surface of the flow, we have
Now, we estimate the length of by adding the length of the pieces for , and the other disjoint arcs. Since , we conclude that
Setting , this proves the proposition. ∎
Next, we reduce to controlling the diameter in . We define
Then, we have the following proposition.
Proposition 6.2.
There exists a constant , such that
(6.3) |
Proof.
For ease of notation, we first analyze the case where the flow has only one conical singularity. After a translation in space-time, we can assume that this singularity is at . Let be the time slice of the tangent flow at this point. By Theorem 5.1, is a graph of function over with norm less than . We can pushforward the metric of to via . Then, the original metric and the pushforward metric of are uniformly equivalent for .
Since is an asymptotically conical shrinker, the family of metrics of is uniformly bounded. Hence, the family of original metrics on is uniformly bounded. This implies that , the length of geodesics , is uniformly bounded by some constant for .
The argument for finitely many conical singularities case is similar. Hence, for , we obtain
where is a constant depending on the asymptotically conical shrinker at as in Theorem 5.1. Choosing , this proves the proposition. ∎
The next step is to reduce to controlling the diameter in neck regions. We first recall the definition of strong -neck and very strong -neck.
Definition 6.3 (strong -neck and very strong -neck).
A mean curvature flow is said to have a strong -neck with center and radius at time if the rescaled flow is -close in sense in to for some . If we can replace the interval by , where is from Proposition 7.1, then we say that has a very strong -neck.
Definition 6.4 (-tube).
is called an -tube if is diffeomorphic to a cylinder, and each lies on the central sphere of a very strong -neck (see Definition 6.3) of with radius at time .
Now, we define
Then, we have the following proposition.
Proposition 6.5 (reduction to neck region).
There exists a constant , such that
(6.4) |
Proof.
Let be a minimizing geodesic in with along , and . According to Theorem 5.1, we know that for small enough, is contained in an -tube possibly with caps as ends, or with its ends identified. Notice that the mean curvatures of the points on the caps are bounded below by . Hence, the caps have diameter bounded by . If the ends of -tube are identified, we only need to remove small controlled pieces and reduce the argument to -tube case. This implies the assertion. ∎
7 Backwards stability and small axis tilt
In this section, we prove Proposition 7.1 (backwards stability) and Proposition 7.2 (small axis tilt). Our backwards stability for necks on the bowl soliton is a special case of what has been observed in more general context for Ricci flow by Kleiner-Lott in [KL17].
Proposition 7.1 (backwards stability).
For all and small enough, we can find with the following property. Suppose is a cylindrical flow or a translating bowl, and has a strong -neck (see Definition 6.3) with center and radius at time . Then, for all , the flow has a strong -neck with center and radius at time .
Proof.
If is a cylindrical flow, after a rotation, we have
for some and .
Because has a strong -neck with center and radius at time , possibly after shifting along the -axis, we get that
(7.1) |
Now, given any , and , we compute
Thanks to (7.1), the terms and can be made arbitrarily small for large enough. This shows that has a strong -neck with radius at time , provided is negative enough (depending only on , ).
If is translating bowl, up to a rotation and translation, we can assume that , where is the graph of function , and is strictly convex and attains its minimum at the origin and has the following asymptotic expansion as (see [CSS07, Lem 2.2]):
(7.2) |
The function is strictly monotone on and has an inverse , where
(7.3) |
Because has a (strong) -neck at time with radius and center , setting , we obtain
(7.4) |
This implies
(7.5) |
Now, for and , using (7.3) and (7.5), we compute,
(7.6) |
Therefore, for any and small enough, we can find large enough, such that if , then has a strong -neck with radius at time . This completes the proof. ∎
Next, we state the proposition about small axis tilt.
Proposition 7.2 ([small axis tilt, [GH17, Prop 4.1]).
Let be a mean curvature flow with entropy bound . For all , there exists , such that if has a strong -neck with center and radius for all time , then has a strong -neck with center , radius and a fixed direction as axis for all time .
This has been proved proof in [GH17, Prop 4.1], using the Lojasiewicz inequality from Coding-Minicozzi [CM15]. Since this is a crucial ingredient for establishing our diameter bound, we include the proof here as well.
Proof.
Consider the renormalized mean curvature flow , where . If is small enough, then we can apply [CM15, Thm 6.1], which gives
(7.7) |
for and some cylinder . Here, are constants, and -functional is defined by
(7.8) |
Applying the discrete Lojasiewicz lemma from [CM15, Lem 6.9] (see also [GH17, A.1]), we infer that for every , as long as is small enough, we have
(7.9) |
By the Cauchy-Schwarz inequality and Huisken’s monontonicty formula, we have
(7.10) |
Using also [CM15, Lemma A.48] and interpolation, this yields the assertion of Proposition 7.2. ∎
8 Completion of the proof
Proof of Theorem 1.4.
Let be a mean curvature flow of closed embedded hypersurfaces in with first singular time , satisfying the assumptions of the theorem. Namely, for every singular point at time , there is some tangent flow which is either a one -factor cylindrical flow or an asymptotically conical flow with multiplicity one.
The following argument depends on various neck-quality parameters . The logical order for choosing these constants is that one first fixes small enough depending only on the dimension, then lets be the constant from Proposition 7.2 and finally chooses given by the claim below. Given any , where is from Theorem 5.1 (decomposition of flow), we want to show that there is a constant independent on , such that
By the Theorem 5.1 (decomposition of flow) and Proposition 6.5 (reduction to neck region), it is enough to estimate
Here, is regularity scale (see Definition 2.8), is from Theorem 5.1, and is an -tube (see Definition 6.4).
For each -tube , we can find an -approximate central curve parametrized by arclength, such that for each , determines the axis of the -neck centered at (see [BHH16]). Then, we only need to estimate the length of .
Note that for any and in the central sphere of the very strong -neck with center and radius at time , and by the definition of regularity scale in Definition 2.8, for small enough, we have that
(8.1) |
Let
(8.2) |
Then, we have the following key claim.
Claim. For small enough, for each in the -approximate curve of the -tube and every , the flow has a strong -neck with center and radius
(8.3) |
at time . Here
(8.4) |
where is the radius of the neck with center at time as above.
Proof of claim.
Suppose towards contradiction, for some fixed , is the largest time such that does not have a strong -neck with center and radius at time .
Because is much smaller than , and has a very strong -neck with center and radius at time , we have . More precisely, let be the constant from Proposition 7.1 (backwards stability). Because is on the central curve of the -tube , the rescaled surface is -close to the surface
in for . Rescaling back it, we infer that the flow
has a strong -neck with center and radius at time , provided that
(8.5) |
Hence, the inequality (8.5) reverses at time . This implies that
(8.6) |
Thus, by the intermediate value theorem, there is some , such that
(8.7) |
By the definition of and since , we know that the flow has a strong -neck with center and radius at time . Let be a point in the central sphere of this neck. We have
(8.8) |
and
(8.9) |
Also, by (8.1) and definition of in (8.2), we have
(8.10) |
Using this and the fact that is a neck point, we see that
(8.11) |
provided is small enough.
Because , we have , where denotes the location of conical singularities in Theorem 5.1. Combining this with the inequality (8.9), we see that
(8.12) |
for all , as long as is small enough. This together with (8.11) and the decomposition (5.1) in Theorem 5.1 implies that
(8.13) |
Hence, by (i)(b) in Theorem 5.1, the flow obtained from by translating to the space-time origin and parabolically rescaling by is -close to a flow that is either a cylindrical flow or a translating bowl.
Since has a strong -neck with center and radius at time , taking also into account (8.8) and (8.9), we see that has a strong -neck with center and radius at time . Applying Proposition 7.1 (backwards stability) on , rescaling by and using again (8.8) and (8.9), we infer that has a strong -neck with center and radius at time as long as
(8.14) |
On the other hand, using (8.7) and the definition of in (8.3), we see that
(8.15) |
so satisfies (8.14). Hence, for small enough, has a strong -neck at with radius at time . This contradiction completes the proof of the claim. ∎
We continue proving Theorem 1.4. By the claim, we can apply Proposition 7.2 (small axis tilt) and obtain that for every , there exists a fixed , such that for all we have that is -close to the cylinder
(8.16) |
in .
Furthermore, as long as , the associated cylinders and will align up to an -error rotation. Then, and . This implies that the intrinsic distance is controlled by extrinsic distance, namely,
(8.17) |
for any two points with .
Noticing that only depends on , , and is covered by controlled number of balls of radius , we conclude that is uniformly bounded in . This completes the proof.
∎
Proof of Theorem 1.5.
We want to prove that there is a constant , such that for , we have
(8.18) |
Using the decomposition (5.1) in Theorem 5.1, we only need to verify the curvature bound in , and . Since the flow has bounded curvature in , the curvature estimation holds in . Hence, we only need to show curvature estimation in and .
For the flow restricted in the mean convex part , by the description of in Theorem 5.1, the flow in can be decomposed into the union of controlled number of -tubes possibly with caps as ends or identified ends. Hence, we only need to estimate curvature bound on each -tube with their possibly cap ends.
Notice that the curvature of the flow in is bounded below by some number , where is from Theorem 5.1 and . This implies that these caps only contribute amount to the curvature integral. On the other hand, for each -tube , by Vitali’s covering lemma, we can write as the union of a maximal collection of -necks with center and radius at time , such that the collection of balls are disjoint. Hence, by Theorem 1.4, we have
(8.19) |
where .
For the flow restricted in the conical part , we estimate the curvature integral in every conical neighborhood , where . Because can be written as graph over with norm less than , where is an asymptotically conical shrinker, we can find a constant , such that
(8.20) |
This completes the proof of Theorem 1.5. ∎
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Department Of Mathematics, University of Toronto, Toronto, ON, M5S 2E4, Canada
E-mail Address: [email protected]