Book 11B

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Course 11Book 11B: Solitons, Compactness and SingularitiesChapter 4

Blow-Ups, Blow-Downs and Splitting at Infinity

Limits of rescaled manifolds and flows: why blow-up limits are nonnegatively curved, what blow-downs see, and how lines appear at infinity.

25 min read · Updated Oct 23, 2026

Read with Morgan and Tian's Ricci Flow and the Poincaré Conjecture, chapter 5, §3–5 (Gromov–Hausdorff convergence and the Tits cone, blow-up limits, splitting limits at infinity), which this chapter follows. Burago, Burago and Ivanov's A Course in Metric Geometry, chapters 7 and 8, is the reference for Gromov–Hausdorff limits of length spaces.

In this chapter · 7 sections
  1. 4.1Gromov–Hausdorff limits of noncompact spaces
  2. 4.2Blowing down: the Tits cone
  3. 4.3Blowing up: limits are nonnegatively curved
  4. 4.4Splitting at infinity
  5. 4.5The asymptotic scalar curvature ratio and dimension reduction
  6. 4.6History
  7. 4.7Exercises
  8. ↗Free resources

The compactness theorem of 11B.3 Compactness of Ricci Flows produces limits of rescaled flows. This chapter is about what those limits look like, in the two directions that Perelman's analysis of singularities uses.

Blowing up, rescaling by a factor that tends to infinity around points of growing curvature, zooms in on a singularity. In dimension three the limits always have nonnegative curvature, by Hamilton–Ivey pinching; this is what makes the theory of κ\kappa-solutions, which assumes nonnegative curvature, applicable to singularities at all.

Blowing down, rescaling by a factor that tends to zero, or equivalently moving the base point off to infinity while rescaling by the distance, looks at a noncompact manifold from far away. For nonnegatively curved manifolds the result is a cone, the asymptotic or Tits cone of 9B.5 Splitting and Soul Theorems, and when the rescaling is at points far out compared with the curvature scale, the limit contains a line and splits off a factor R\mathbb{R}. This splitting at infinity is how Perelman shows that the far parts of κ\kappa-solutions look like necks, and it is one of the main uses of the splitting theorem.

By the end of this chapter you will be able to:

  • define pointed Gromov–Hausdorff convergence of noncompact length spaces, with δ\delta-nets, and give the standard examples;
  • define the Tits cone of a nonnegatively curved manifold, and state that blow-downs converge to it;
  • define blow-up limits of sequences of flows, and prove that in dimension three they have nonnegative curvature;
  • prove that if a nonnegatively curved manifold is rescaled at points going to infinity, faster than their distance from a fixed point, any smooth limit splits off a line;
  • define the asymptotic scalar curvature ratio and state Hamilton's dimension reduction, and explain how these produce necks.

Gromov–Hausdorff limits of noncompact spaces

9B.4 Convergence of Manifolds defined the Gromov–Hausdorff distance between compact metric spaces. For noncompact spaces, which is the situation of every blow-up and blow-down, one uses base points and balls.

Definition 4.1 Pointed Gromov–Hausdorff convergence

Based metric spaces (Xk,xk)(X_k, x_k) converge to (Y,y)(Y, y) if for every r>0r > 0 there are δk→0\delta_k \to 0 such that the balls B(xk,r+δk)B(x_k, r + \delta_k), based at xkx_k, converge in the Gromov–Hausdorff sense to the ball B(y,r)B(y, r) based at yy.

A δ\delta-net in (X,x)(X, x) is a subset L∋xL \ni x, uniformly discrete, whose δ\delta-neighbourhood is all of XX; a maximal subset whose δ2\frac\delta2-balls are disjoint is one. Convergence can be tested on nets: (Xk,xk)→(X,x)(X_k, x_k) \to (X, x), for uniformly bounded spaces, exactly when every finite net of XX is approximated, up to bi-Lipschitz distortion tending to 11, by nets of the XkX_k (Morgan and Tian's Lemma 5.22, citing Gromov). Limits that are complete and locally compact are unique up to isometry of based spaces. For length spaces, in which distances are realised by curves, there is a precompactness criterion of the kind proved in 9B.4 Convergence of Manifolds: a sequence has a convergent subsequence if, for every δ\delta and RR, the number of disjoint δ\delta-balls in B(xk,R)B(x_k, R) is bounded independently of kk (Morgan and Tian's Theorem 5.28). By Bishop–Gromov this holds whenever the Ricci curvature is bounded below uniformly, so every sequence with Ric⁡≥−(n−1)Λ\operatorname{Ric} \geq -(n - 1)\Lambda has Gromov–Hausdorff convergent subsequences, possibly to singular or lower-dimensional limits.

Examples: round cylinders Sn−1(ρk)×RS^{n-1}(\rho_k)\times\mathbb{R} with ρk→0\rho_k \to 0 converge, from any base points, to the line R\mathbb{R}; the thin tori of 9B.3 Collapsing and Noncollapsing converge to a circle; and rescalings λk−2g\lambda_k^{-2}g of the Euclidean metric, with any λk\lambda_k, are all isometric to it. Gromov–Hausdorff limits forget smoothness; geometric (Cheeger–Gromov) limits, which need curvature and injectivity radius bounds (9B.4 Convergence of Manifolds, 11B.3 Compactness of Ricci Flows), keep it. In what follows both kinds appear, and the art is to use the weaker one where the stronger is not available.

Blowing down: the Tits cone

Let (M,g)(M, g) be complete, noncompact, with nonnegative sectional curvature, and p∈Mp \in M. For two rays γ\gamma, μ\mu from pp (minimising unit-speed geodesics [0,∞)→M[0, \infty) \to M, 9B.5 Splitting and Soul Theorems), Toponogov's theorem (9B.5 Splitting and Soul Theorems) shows that the comparison angle at pp of the triangle p,γ(r),μ(r)p, \gamma(r), \mu(r), the Euclidean angle with the same three side lengths, is a nonincreasing function of rr. Its limit θ∞(γ,μ)\theta_\infty(\gamma, \mu) is the angle at infinity between the rays.

Definition 4.2 The Tits cone

Identify rays from pp with angle at infinity 00. The set of classes, with the distance θ∞\theta_\infty, is a compact length space S∞(M,p)S_\infty(M, p) of diameter at most π\pi, the space of directions at infinity. The Tits cone T(M,p)T(M, p) is the Euclidean cone over it: S∞×[0,∞)S_\infty\times[0, \infty) with S∞×{0}S_\infty\times\{0\} collapsed to a vertex, and distance d((ξ,s),(η,u))2=s2+u2−2sucos⁡θ∞(ξ,η)d\big((\xi, s), (\eta, u)\big)^2 = s^2 + u^2 - 2su\cos\theta_\infty(\xi, \eta).

Theorem 4.3 Blow-downs converge to the Tits cone (statement)

For (M,g)(M, g) complete, noncompact, with K≥0K \geq 0, and λk→∞\lambda_k \to \infty, the rescaled spaces (M,λk−2g,p)(M, \lambda_k^{-2}g, p) converge in the pointed Gromov–Hausdorff sense to T(M,p)T(M, p), based at the vertex.

The idea: a point at distance λks\lambda_ks from pp on a ray γ\gamma becomes the point (γ,s)(\gamma, s) after rescaling, and by Toponogov the rescaled distance between two such points converges to the cone distance, because the comparison angle converges to θ∞\theta_\infty. Every point far away is close, on the rescaled scale, to a point on some ray (Morgan and Tian's Proposition 5.31). Examples (9B.5 Splitting and Soul Theorems): the paraboloid blows down to a ray, Rn\mathbb{R}^n to itself, a round cylinder S2×RS^2\times\mathbb{R} to a line, and the Bryant soliton, whose cross-sections grow like s\sqrt s, to a ray: its spheres at distance ss have radius about s\sqrt s, which is negligible compared with ss.

The dimension of the Tits cone measures the asymptotic volume ratio of 9B.2 Volume Comparison: the cone is nn-dimensional exactly when the volume of large balls grows like rnr^n. Perelman proves that a κ\kappa-solution has asymptotic volume ratio 00 (12B.3 The Structure of κ-Solutions); the proof combines the blow-down with the no-cones proposition of 11A.8 The Strong Maximum Principle and Splitting: if the ratio were positive, a blow-down of the flow would be a smooth flow through a nonflat cone with nonnegative curvature, which is impossible.

Blowing up: limits are nonnegatively curved

Definition 4.4 Blow-up limits

Let (Mk,gk(t),xk)(M_k, g_k(t), x_k) be a sequence of Ricci flows (or flows with surgery) with Qk=R(xk,tk)→∞Q_k = R(x_k, t_k) \to \infty. Shift time so that tk=0t_k = 0 and rescale: g~k(s)=Qkgk(s/Qk)\tilde g_k(s) = Q_kg_k(s/Q_k), so that R~(xk,0)=1\tilde R(x_k, 0) = 1. If a subsequence converges geometrically to a Ricci flow (M∞,g∞(s),x∞)(M_\infty, g_\infty(s), x_\infty), s∈(−T,0]s \in (-T, 0], that limit is a blow-up limit; if only the time-zero slices converge, the limit of those is a blow-up limit of the zero time slices.

The point of normalising by R(xk)R(x_k) rather than ∣Rm⁡∣(xk)|\operatorname{Rm}|(x_k) is that RR is the quantity the canonical neighbourhood theorem is phrased in, and in dimension three, by pinching, the two are comparable where they are large.

Theorem 4.5 Blow-up limits are nonnegatively curved (Morgan–Tian, Theorem 5.33)

Let (Mk,gk(t))(M_k, g_k(t)) be three-dimensional Ricci flows (or generalised flows) with curvature pinched toward positive in the sense of Hamilton–Ivey: R≥−64t+1R \geq -\frac{6}{4t + 1}, and wherever the smallest eigenvalue ν\nu of the curvature operator is negative, R≥∣ν∣(log⁡∣ν∣+log⁡(1+t)−3)R \geq |\nu|\big(\log|\nu| + \log(1 + t) - 3\big). If Qk=R(xk,tk)→∞Q_k = R(x_k, t_k) \to \infty, every blow-up limit, and every blow-up limit of the zero time slices, has nonnegative curvature operator.

Proof. Let yy be a point of the limit at some time ss, and yky_k points of the rescaled flows converging to it. Let λ≥μ≥ν\lambda \geq \mu \geq \nu denote eigenvalues of the curvature operator. The limit's eigenvalues at yy are lim⁡Qk−1λ(yk)\lim Q_k^{-1}\lambda(y_k), lim⁡Qk−1μ(yk)\lim Q_k^{-1}\mu(y_k), lim⁡Qk−1ν(yk)\lim Q_k^{-1}\nu(y_k) (curvature scales by Qk−1Q_k^{-1}). First, R≥−6R \geq -6 before rescaling (the lower bound −64t+1-\frac{6}{4t + 1} is at least −6-6), so Qk−1R(yk)→R(y)≥0Q_k^{-1}R(y_k) \to R(y) \geq 0. If λ(y)=0\lambda(y) = 0, then R(y)≥0R(y) \geq 0 forces all eigenvalues of the limit at yy to vanish (μ,ν≤λ=0\mu, \nu \leq \lambda = 0 and λ+μ+ν≥0\lambda + \mu + \nu \geq 0), and the curvature is 0≥00 \geq 0. Otherwise λ(yk)→∞\lambda(y_k) \to \infty. Two cases. If ν(yk)\nu(y_k) stays bounded below, then Qk−1ν(yk)Q_k^{-1}\nu(y_k) has a limit ≥0\geq 0, and so does Qk−1μ(yk)≥Qk−1ν(yk)Q_k^{-1}\mu(y_k) \geq Q_k^{-1}\nu(y_k): the limit is nonnegative at yy. If ν(yk)→−∞\nu(y_k) \to -\infty, pinching gives ∣ν(yk)∣R(yk)≤1log⁡∣ν(yk)∣−3→0\frac{|\nu(y_k)|}{R(y_k)} \leq \frac{1}{\log|\nu(y_k)| - 3} \to 0, while Qk−1R(yk)Q_k^{-1}R(y_k) converges to the finite R(y)R(y); so Qk−1∣ν(yk)∣=∣ν(yk)∣R(yk)⋅Qk−1R(yk)→0Q_k^{-1}|\nu(y_k)| = \frac{|\nu(y_k)|}{R(y_k)}\cdot Q_k^{-1}R(y_k) \to 0, the limit has ν(y)=0\nu(y) = 0, and μ(y)≥ν(y)=0\mu(y) \geq \nu(y) = 0. In every case the limit's curvature operator is nonnegative at yy.

Hamilton–Ivey pinching holds for every Ricci flow on a closed 3-manifold after normalising the initial metric (11A.10 Hamilton–Ivey Pinching, 11A.9 Flows on Complete Manifolds), and Perelman arranges that it survives surgery (12B.9 Surgery), so the theorem applies to every flow in the proof of the Poincaré conjecture. This is the reason three dimensions are special for the singularity analysis: in higher dimensions blow-up limits can have curvature of both signs.

Splitting at infinity

Theorem 4.6 Splitting limits at infinity (Morgan–Tian, Theorem 5.35)

Let (M,g)(M, g) be complete and connected with nonnegative sectional curvature, xn→∞x_n \to \infty in MM, and λn>0\lambda_n > 0 such that (M,λng,xn)(M, \lambda_ng, x_n) has a geometric limit (M∞,g∞,x∞)(M_\infty, g_\infty, x_\infty). Suppose that for some p∈Mp \in M, λnd(p,xn)2→∞\lambda_nd(p, x_n)^2 \to \infty. Then minimising geodesics from xnx_n to pp converge, after passing to a subsequence, to a ray in M∞M_\infty that is half of a line, and M∞M_\infty splits isometrically as N×RN\times\mathbb{R}.

Proof. Write dn=d(p,xn)→∞d_n = d(p, x_n) \to \infty, and let γn\gamma_n be minimising geodesics from pp to xnx_n.

Nearly aligned directions. The initial unit vectors of the γn\gamma_n at pp lie in a compact sphere, so after passing to a subsequence they converge. Given δ∈(0,1)\delta \in (0, 1) there is NN such that for n,m≥Nn, m \geq N the angle at pp between γn\gamma_n and γm\gamma_m is less than δ\delta. For each such nn choose m(n)≥Nm(n) \geq N with dm(n)≥dn(1+1δ)d_{m(n)} \geq d_n(1 + \frac1\delta), which is possible as dm→∞d_m \to \infty, and let μn\mu_n be a minimising geodesic from xnx_n to xm(n)x_{m(n)}, of length ℓn\ell_n.

The angle at xnx_n is nearly straight. By Toponogov's hinge comparison (9B.5 Splitting and Soul Theorems) at pp, with angle less than δ\delta, ℓn2≤dn2+dm(n)2−2dndm(n)cos⁡δ\ell_n^2 \leq d_n^2 + d_{m(n)}^2 - 2d_nd_{m(n)}\cos\delta, and by the triangle inequality ℓn≥dm(n)−dn\ell_n \geq d_{m(n)} - d_n. Let θn\theta_n be the angle at xnx_n in the Euclidean comparison triangle with sides dnd_n, ℓn\ell_n, dm(n)d_{m(n)}. By the law of cosines,

cos⁡θn=dn2+ℓn2−dm(n)22dnℓn≤2dn2−2dndm(n)cos⁡δ2dnℓn=dnℓn−dm(n)ℓncos⁡δ.\cos\theta_n = \frac{d_n^2 + \ell_n^2 - d_{m(n)}^2}{2d_n\ell_n} \leq \frac{2d_n^2 - 2d_nd_{m(n)}\cos\delta}{2d_n\ell_n} = \frac{d_n}{\ell_n} - \frac{d_{m(n)}}{\ell_n}\cos\delta.

Since ℓn≥dm(n)−dn≥dnδ\ell_n \geq d_{m(n)} - d_n \geq \frac{d_n}{\delta}, we have dnℓn≤δ\frac{d_n}{\ell_n} \leq \delta; and by the triangle inequality dm(n)≥ℓn−dnd_{m(n)} \geq \ell_n - d_n, so dm(n)ℓn≥1−dnℓn≥1−δ\frac{d_{m(n)}}{\ell_n} \geq 1 - \frac{d_n}{\ell_n} \geq 1 - \delta. So cos⁡θn≤δ−(1−δ)cos⁡δ\cos\theta_n \leq \delta - (1 - \delta)\cos\delta, which tends to −1-1 as δ→0\delta \to 0: the comparison angle at xnx_n between the segment back to pp and the segment on to xm(n)x_{m(n)} tends to π\pi. Toponogov's theorem (the angle comparison form) says the actual angle is at least the comparison angle, and more: for points at distances α≤dn\alpha \leq d_n along γn\gamma_n (back towards pp) and β≤ℓn\beta \leq \ell_n along μn\mu_n from xnx_n, their distance is at least α2+β2−2αβcos⁡θn\sqrt{\alpha^2 + \beta^2 - 2\alpha\beta\cos\theta_n}, which is nearly α+β\alpha + \beta.

Passing to the limit. In the rescaled metrics λng\lambda_ng, the lengths λndn→∞\sqrt{\lambda_n}d_n \to \infty by hypothesis and λnℓn≥λndnδ→∞\sqrt{\lambda_n}\ell_n \geq \sqrt{\lambda_n}\frac{d_n}{\delta} \to \infty too. The geodesics γn\gamma_n (reversed, starting at xnx_n) and μn\mu_n, as maps from intervals of length tending to infinity, converge on compact sets, after passing to a subsequence, to two rays γ∞\gamma_\infty, μ∞\mu_\infty from x∞x_\infty in M∞M_\infty: geodesics in the converging metrics converge to geodesics, and minimising ones to minimising ones. In the limit the distance estimate becomes d∞(γ∞(α),μ∞(β))≥α+βd_\infty(\gamma_\infty(\alpha), \mu_\infty(\beta)) \geq \alpha + \beta, with equality by the triangle inequality through x∞x_\infty. So γ∞\gamma_\infty followed by μ∞\mu_\infty is a line through x∞x_\infty.

Splitting. M∞M_\infty is a smooth limit of manifolds with nonnegative sectional curvature, so it has nonnegative sectional curvature, in particular Ric⁡≥0\operatorname{Ric} \geq 0; it is complete; and it contains a line. By the splitting theorem (9B.5 Splitting and Soul Theorems) M∞=N×RM_\infty = N\times\mathbb{R} isometrically, with the line a factor line {x}×R\{x\}\times\mathbb{R}.

The hypothesis λnd(p,xn)2→∞\lambda_nd(p, x_n)^2 \to \infty says that, on the scale at which we look (λn−1/2\lambda_n^{-1/2}), the point pp recedes to infinity. Seen from xnx_n, there is a long segment back to pp and, by the choice of xm(n)x_{m(n)}, a long segment onwards, and nonnegative curvature forces them to line up. For a cylinder the conclusion is evident at every scale; for the paraboloid z=x2+y2z = x^2 + y^2 at a large distance dd from the vertex, the circles of revolution have radius about d\sqrt d; rescaling by their width, λ=1d\lambda = \frac1d, makes them of radius about 11, and λd2=d→∞\lambda d^2 = d \to \infty, so the limit is a flat cylinder S1(1)×RS^1(1)\times\mathbb{R}, with the line along the axis: far out, at the scale of its own width, the paraboloid looks like a cylinder.

The asymptotic scalar curvature ratio and dimension reduction

How the curvature decays at infinity, compared with the distance, decides which kind of rescaling sees a splitting. For a complete noncompact (M,g)(M, g) and p∈Mp \in M, the asymptotic scalar curvature ratio is

R=lim sup⁡x→∞R(x) d(p,x)2,\mathcal R = \limsup_{x \to \infty}R(x)\,d(p, x)^2,

independent of pp. It is scale-invariant. Examples: R=0\mathcal R = 0 for flat space and for the cigar (curvature decays exponentially); R=∞\mathcal R = \infty for the cylinder S2×RS^2\times\mathbb{R} (curvature constant); for the two-dimensional paraboloid, whose circles have radius about d\sqrt d at distance dd, the Gauss curvature is about 14d2\frac{1}{4d^2} and R=12\mathcal R = \frac12, finite; for the three-dimensional Bryant soliton, whose cross-sectional spheres have radius about d\sqrt d, R∼cdR \sim \frac cd and R=∞\mathcal R = \infty.

When R=∞\mathcal R = \infty, there are points xn→∞x_n \to \infty with R(xn)d(p,xn)2→∞R(x_n)d(p, x_n)^2 \to \infty, and rescaling by λn=R(xn)\lambda_n = R(x_n) satisfies the hypothesis of Theorem 4.6. If the rescaled manifolds converge (which needs curvature bounds near xnx_n at the scale R(xn)−1/2R(x_n)^{-1/2}, arranged by point picking as in 11B.5 Singularities, and an injectivity radius bound, supplied by noncollapsing), the limit splits off a line. Hamilton called this dimension reduction (1995): an ancient solution with nonnegative curvature and R=∞\mathcal R = \infty has blow-up limits at infinity of the form Nn−1×RN^{n-1}\times\mathbb{R} (statement here; Morgan and Tian, chapter 9, §3, carry it out for κ\kappa-solutions). In dimension three, NN is a surface, and the two-dimensional theory (a noncollapsed ancient solution on a surface with positive curvature is a round sphere, 12B.1 κ-Solutions) identifies N×RN\times\mathbb{R} as the round cylinder. That is how necks are found far out on κ\kappa-solutions.

When R\mathcal R is finite, blow-downs by the distance see a cone, and the analysis goes through Theorem 4.3 and the no-cones proposition of 11A.8 The Strong Maximum Principle and Splitting instead. Perelman shows that for a noncompact κ\kappa-solution the asymptotic volume ratio is zero and R=∞\mathcal R = \infty, so that the dimension reduction always applies (12B.3 The Structure of κ-Solutions).

Where this goes Where these limits are used

11B.5 Singularities produces blow-up limits at singularities; this chapter shows they are nonnegatively curved. 12B.1 κ-Solutions and 12B.3 The Structure of κ-Solutions use blow-downs, the Tits cone and splitting at infinity to analyse κ\kappa-solutions, and 12B.5 The Canonical Neighbourhood Theorem blows up at points of high curvature in a general flow to prove the canonical neighbourhood theorem.

History

Gromov introduced the Gromov–Hausdorff distance and its pointed version around 1980 and proved the precompactness criterion in 1981. The angle comparison behind the Tits cone is Toponogov's (1959); the cone at infinity of nonnegatively curved manifolds was studied by Ballmann, Gromov and Schroeder, among others, in the 1980s. Hamilton's dimension reduction and the asymptotic scalar curvature ratio are from "The formation of singularities in the Ricci flow" (1995). Perelman used splitting at infinity throughout his analysis of κ\kappa-solutions (2002), and Morgan and Tian's chapter 5 states it in the form proved here.

Recall Where we stand

Noncompact spaces converge in the pointed Gromov–Hausdorff sense when balls do; lower Ricci bounds make every sequence precompact, and limits may be singular or lower-dimensional (cylinders collapse to a line). A nonnegatively curved manifold, blown down, converges to its Tits cone, the cone over its directions at infinity. Blow-up limits of three-dimensional flows pinched toward positive have nonnegative curvature, because Hamilton–Ivey makes negative curvature negligible where curvature is large. Rescaling a nonnegatively curved manifold at points xnx_n with λnd(p,xn)2→∞\lambda_nd(p, x_n)^2 \to \infty makes the segment back to pp and a segment onwards line up (Toponogov), so smooth limits contain a line and split. When the asymptotic scalar curvature ratio is infinite, blow-ups at infinity split off a line (dimension reduction), and in three dimensions they are necks. 11B.5 Singularities studies singularities.

Exercises

Exercise 4.7 Cylinders collapse to a line

Show directly that S1(ρ)×RS^1(\rho)\times\mathbb{R}, based at any point, converges to (R,0)(\mathbb{R}, 0) in the pointed Gromov–Hausdorff sense as ρ→0\rho \to 0, by exhibiting correspondences between balls with distortion tending to zero.

Solution

Relate (θ,s)(\theta, s) to ss. For two points, d2=dS1(θ,θ′)2+(s−s′)2d^2 = d_{S^1}(\theta, \theta')^2 + (s - s')^2 with dS1≤πρd_{S^1} \leq \pi\rho, so 0≤d−∣s−s′∣≤πρ0 \leq d - |s - s'| \leq \pi\rho. The correspondence between B((θ0,0),r)B((\theta_0, 0), r) and (−r,r)(-r, r) (up to the small adjustment at the boundary in the definition) has distortion at most πρ→0\pi\rho \to 0, so the Gromov–Hausdorff distance between the balls is at most πρ2+o(1)\frac{\pi\rho}{2} + o(1).

Exercise 4.8 Angles at infinity on the paraboloid

For the paraboloid z=x2+y2z = x^2 + y^2 and pp its vertex, show that any two rays from pp have angle at infinity 00, so the Tits cone is a ray. (Hint: points at distance rr from pp along two rays are at distance O(r)O(\sqrt r) from each other, being on a circle of radius about r\sqrt r.)

Solution

Far out, the paraboloid is a surface of revolution whose circles at height zz have radius z\sqrt z, and the distance from the vertex is about zz. Two rays (meridians) from the vertex at distance rr are on the circle of radius about r\sqrt r, so their distance is at most πr\pi\sqrt r. The Euclidean comparison triangle with sides rr, rr and at most πr\pi\sqrt r has angle at pp at most about πrr→0\frac{\pi\sqrt r}{r} \to 0. So all angles at infinity vanish, S∞S_\infty is a point, and the Tits cone is the cone over a point: a ray.

Exercise 4.9 The role of pinching

Give an example of a sequence of complete 3-manifolds (not Ricci flows) with R(xk)→∞R(x_k) \to \infty whose rescalings by R(xk)R(x_k) converge to a manifold with some negative sectional curvature, and explain why it is not a counterexample to Theorem 4.5.

Solution

Take Mk=S2(ρk)×ΣkM_k = S^2(\rho_k)\times\Sigma_k, a product of a round sphere of radius ρk\rho_k with a complete hyperbolic surface of curvature −12ρk2-\frac{1}{2\rho_k^2}, as ρk→0\rho_k \to 0. The scalar curvature is 2ρk2−1ρk2=1ρk2→∞\frac{2}{\rho_k^2} - \frac{1}{\rho_k^2} = \frac{1}{\rho_k^2} \to \infty. Rescaling by R=ρk−2R = \rho_k^{-2} gives, for every kk, S2(1)×ΣS^2(1)\times\Sigma with Σ\Sigma of curvature −12-\frac12: a constant sequence, whose limit has sectional curvature −12-\frac12 on the planes tangent to Σ\Sigma. The sequence violates Hamilton–Ivey pinching, since ∣ν∣|\nu| is comparable to RR at arbitrarily large RR; it cannot arise in a Ricci flow on a closed 3-manifold with normalised initial data, for which the theorem's hypothesis holds.

Exercise 4.10 The cigar has R=0\mathcal R = 0

Compute the asymptotic scalar curvature ratio of the cigar ds2+tanh⁡2s dθ2ds^2 + \tanh^2s\,d\theta^2 and of the Bryant soliton (using R∼csR \sim \frac cs). Which of them can be blown up at infinity to produce a splitting, and what is the limit in each case?

Solution

For the cigar R=4sech⁡2s≈16e−2sR = 4\operatorname{sech}^2s \approx 16e^{-2s}, so R d2≈16s2e−2s→0R\,d^2 \approx 16s^2e^{-2s} \to 0: R=0\mathcal R = 0. Rescaling far out by λn=R(xn)→0\lambda_n = R(x_n) \to 0 shrinks the cylindrical end of circumference 2π2\pi to nothing: the Gromov–Hausdorff limit is a line, collapsed, and there is no smooth limit. For the Bryant soliton, R d2∼cs→∞R\,d^2 \sim cs \to \infty: R=∞\mathcal R = \infty. Rescaling by R(xn)≈csnR(x_n) \approx \frac{c}{s_n} at xnx_n far out makes the cross-sectional spheres, of radius about sn\sqrt{s_n}, of size about 11, and the limit is the round cylinder S2×RS^2\times\mathbb{R}: a neck, with the line along the axis.

Exercise 4.11 Rehearsal: necks far out on a capped cylinder

Let (M,g)(M, g) be a complete surface of revolution in R3\mathbb{R}^3 with K≥0K \geq 0 that is asymptotic to a round cylinder of radius 11 (a capped cylinder), times a line: M×RM\times\mathbb{R} is then a complete 3-manifold with K≥0K \geq 0. Taking λn=1\lambda_n = 1 and xnx_n going out along the cylindrical end, check the hypothesis of Theorem 4.6 and identify the limit. Then explain why rescaling by λn→0\lambda_n \to 0 at the same points gives a Gromov–Hausdorff limit that is a plane, not a smooth 3-manifold.

Solution

λnd(p,xn)2=d(p,xn)2→∞\lambda_nd(p, x_n)^2 = d(p, x_n)^2 \to \infty. The pointed limit at the scale 11 is the round cylinder S1(1)×RS^1(1)\times\mathbb{R} times the extra R\mathbb{R}, that is S1×R2S^1\times\mathbb{R}^2; it contains the line along the cylinder's axis, and it splits off two lines in fact. Rescaling by λn→0\lambda_n \to 0 shrinks the circle factor to nothing, so the Gromov–Hausdorff limit is R2\mathbb{R}^2, of lower dimension; no smooth limit of dimension three exists, because the injectivity radius at xnx_n tends to zero in the rescaled metrics (collapse, 9B.3 Collapsing and Noncollapsing).

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