Structures with adaptive cooling

Patent metadata

Field	Value
Publication number	US-9587832-B2
Application number	US-28670508-A
Country	US
Kind code	B2
Filing date	Oct 1, 2008
Priority date	Oct 1, 2008
Publication date	Mar 7, 2017
Grant date	Mar 7, 2017

Abstract

Disclosed are exemplary structures with adaptive cooling and methods of adaptively cooling structures. A liner is affixed to a support and the liner deflects away from the support when exposed to a localized hot spot in a hot fluid stream. The liner deflection creates a chamber between the liner and support, allowing cooling air to impinge against the liner, thus mitigating the effects of the hot spot. By providing impingement cooling only where needed, the amount of air needed for cooling is reduced.

First claim

What is claimed is:

1. A structure with adaptive cooling comprising:
a mounting support having a coolant aperture for directing cooling air through said support; and
a liner mounted to said support, said liner including a wall having a hot surface facing away from said support and a cold surface facing toward said support, said liner having:
an average temperature position, wherein said liner wall cold surface contacts said mounting support, said liner wall cold surface defining a channel sufficiently proximate said coolant aperture to permit a convective flow of cooling air from said coolant aperture; and
a hot temperature position induced by a hot spot location on said liner wall hot surface, wherein said liner wall deflects away from said mounting support to form a chamber between said liner wall cold surface and said mounting support, said chamber having an offset distance from the coolant aperture to the liner wall cold surface sufficient to permit said cooling air to impinge on the cold surface of said liner wall.

2. The structure of claim 1 , wherein said liner has a film aperture through the wall and the cooling air passes through the film aperture and exits the hot surface, forming a film.

3. The structure of claim 1 , wherein said liner wall is porous and the cooling air passes through the pores and exits the hot surface, forming a film.

4. The structure of claim 3 , wherein the channel is defined by a texture on the cold surface of said liner.

5. The structure of claim 2 , wherein the liner is mounted to the support with fastening means.

6. The structure of claim 2 , wherein the support further comprises an array of coolant apertures and the liner wall further comprises an array of film apertures.

7. The structure of claim 1 , wherein the coolant apertures have a diameter D, and said liner wall deflects away from the support a distance L that is between approximately one to five times the value of D, L being defined at a point offset from a maximum deflection point.

8. The structure of claim 7 , wherein said liner wall deflects away from the support a distance L that is between approximately two to four times the value of D.

9. The structure of claim 8 , wherein said liner wall deflects away from the support a distance L that is approximately three times the value of D.

10. A method of adaptively cooling a liner mounted to a support comprising:
providing a support having a coolant aperture;
providing a liner mounted to the support, the liner including a wall having a hot surface facing away from the support and a cold surface facing toward the support, the liner wall cold surface defining a channel;
introducing cooling air into a coolant aperture in the support;
directing the cooling air through the coolant aperture and into the channel;
placing the liner in an average temperature position in which the liner wall cold surface contacts the support, wherein the channel is sufficiently proximate said coolant aperture to permit a convective flow of cooling air from said coolant aperture; and
deflecting the liner to a hot temperature position in response to a hot spot location on said liner wall hot surface in which the liner wall is spaced from the support to form a chamber between the liner wall cold surface and the support, wherein the chamber has an offset distance from the coolant aperture to the liner wall cold surface sufficient to permit the cooling air to impinge on the liner wall cold surface.

11. The method of claim 10 wherein the coolant aperture has a diameter D, and the deflecting step causes the liner to deflect a distance L that is between approximately one to five times the value of D away from the support, L being defined at a point offset from a maximum deflection point.

12. The method of claim 11 wherein the coolant aperture has a diameter D, and the deflecting step causes the liner to deflect a distance L that is between approximately two to four times the value of D away from the support.

13. The method of claim 11 wherein the coolant aperture has a diameter D, and the deflecting step causes the liner to deflect a distance L that is between approximately three times the value of D away from the support.

14. The method of claim 10 further comprising the step of directing the cooling air into an aperture in the liner.

15. The method of claim 10 further comprising the step of directing the cooling air into pores in the liner.

Assignees

• Dierberger James A
• United Technologies Corp

Inventors

• Dierberger James A

Classifications

• F23R2900/03044

  Impingement cooled combustion chamber walls or subassemblies · CPC title

• Y02T50/67

  Cross-Sectional Technologies · mapped topic

• F23R3/04 Primary

  Air inlet arrangements · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F23R3/002

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title