Enhanced impingement cooled components

• US 5,353,865 A
• Filed: 03/30/1992
• Issued: 10/11/1994
• Est. Priority Date: 03/30/1992
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Adiutori, Eugene F., Aleshin, Stephen, Pritchard, Byron A. Jr.
• Primary Examiner(s): Flanigan, Allen J.
• Application Number:
  US07/860,397
• Time in Patent Office: 925 Days
• Field of Search: 165/133, 165/185, 165/109.1, 165/908, 138/38
• US Class Current: 165/133
• CPC Class Codes: F23R 2900/03044 Impingement cooled combustion chamber walls or subassemblies
• CPC Class Codes: F23R 2900/03045 Convection cooled combustion chamber walls provided with turbolators or means for creating turbulences to increase cooling
• CPC Class Codes: F28F 13/02 by influencing fluid boundary boundary-layer control in general F15D
• CPC Class Codes: F28F 13/185 Heat-exchange surfaces provided with microstructures or with porous coatings
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10S 165/908 Fluid jets

Abstract

An improved heat transfer assembly includes a textured impingement surface and means for impinging cooling air directly upon the textured surface. A component includes a surface textured to increase convective heat transfer with minimal increase in resistance to conductive heat transfer through the component. The textured surface can comprise an array of closely spaced hemispherically shaped protuberances. A method is disclosed for texturing a surface with discrete laser welds.

Claims

1. An improved component heat transfer assembly for use in a gas turbine engine, the assembly comprising:

a. a component including a textured surface; and

b. impingement means spaced from the textured surface for directing an impinging fluid to directly impinge upon the textured surface; and

c. wherein the textured surface comprises an array of protuberances extending from a first surface and wherein the impingement means is spaced from the protuberances for directing an impinging fluid to directly impinge upon a plurality of the protuberances;

d. wherein the protuberances are generally semi-spherical in shape.

2. An improved component heat transfer assembly for use in a gas turbine engine, the assembly comprising:

a. a component including a textured surface; and

b. impingement means spaced from the textured surface for directing an impinging fluid to directly impinge upon the textured surface; and

c. wherein the textured surface comprises an array of protuberances extending from a first surface and wherein the impingement means is spaced from the protuberance for directing an impinging fluid to directly impinge upon a plurality of the protuberances;

d. wherein the protuberances are generally hemispherical in shape.

3. An improved component heat transfer assembly for use in a gas turbine engine, the assembly comprising:

a. a component including a textured surface; and

b. impingement means spaced from the textured surface for directing an impinging fluid to directly impinge upon the textured surface; and

c. wherein the textured surface comprises an array of protuberances extending from a first surface and wherein the impingement means is spaced from the protuberances for directing an impinging fluid to directly impinge upon a plurality of the protuberances;

d. wherein the protuberances are generally hemispherical in shape and wherein the protuberances extend above the first surface with a height less than or equal to 0.020 inch.

4. The assembly of claim 3 wherein a protuberance-to-protuberance spacing of the protuberances on the first surface is less than two times the diameter of the protuberances.

5. An improved component heat transfer assembly for use in a gas turbine engine, the assembly comprising:

a. a component including a textured surface; and

b. impingement means spaced from the textured surface for directing an impinging fluid to directly impinge upon the textured surface; and

c. wherein the textured surface comprises an array of protuberances extending from a first surface and wherein the impingement means is spaced from the protuberances for directing an impinging fluid to directly impinge upon a plurality of the protuberances;

d. wherein the protuberances are discrete hemispherical weld beads disposed on the first surface.