Airfoil impingement cavity

Patent metadata

Field	Value
Publication number	US-2016333701-A1
Application number	US-201514710397-A
Country	US
Kind code	A1
Filing date	May 12, 2015
Priority date	May 12, 2015
Publication date	Nov 17, 2016
Grant date	—

Abstract

An airfoil having one-sided pedestals is disclosed. The airfoil may define various cavities, such as an inflow feed cavity, an impingement cavity, and an outflow cavity. The various cavities may be connected by crossover sections such as an inflow crossover section and an outflow crossover section. Cooling air may be conducted into the inflow feed cavity, out of the inflow feed cavity through an inflow crossover section into an impingement cavity, and through an impingement cavity. The cooling air may be conducted out of the impingement cavity and into an outflow cavity through an outflow crossover section. Various cavities may include one-wall pedestals. One-wall pedestals may be structures extending from a wall of a cavity into the void of the cavity, whereupon cooling air may impinge, effectuating convective cooling.

First claim

1 . An airfoil comprising:
a first feed cavity defined within a body of the airfoil and configured to receive cooling air; a first impingement cavity defined within the body of the airfoil and comprising a one-wall pedestal; a first inflow crossover section defined within the body of the airfoil and configured to conduct the cooling air from the first feed cavity to the first impingement cavity, wherein the one-wall pedestal comprises a boss extending from a surface of the first impingement cavity and into a void defined by a boundary of the first impingement cavity.

2 . The airfoil according to claim 1 , wherein the one-wall pedestal comprises a round boss.

3 . The airfoil according to claim 1 , wherein the one-wall pedestal comprises a trapezoidal boss.

4 . The airfoil according to claim 1 , wherein the one-wall pedestal comprises a triangular boss.

5 . The airfoil according to claim 1 , wherein the one-wall pedestal comprises an oval boss.

6 . The airfoil according to claim 1 , wherein the one-wall pedestal comprises a round boss having a height (H) and a diameter (D) defined according to a ratio wherein 0.25<=H/D<=4.0.

7 . The airfoil according to claim 1 , wherein the one-wall pedestal has a height and an effective hydraulic diameter defined according to a ratio wherein 0.25<=height/effective hydraulic diameter <=4.0.

8 . The airfoil according to claim 1 , wherein the first inflow crossover section comprises a linear crossover channel.

9 . The airfoil according to claim 1 , wherein the first inflow crossover section comprises a staggered crossover channel.

10 . The airfoil according to claim 1 , wherein the airfoil comprises a first outflow crossover section defined within the body of the airfoil and configured to conduct the cooling air away from the first impingement cavity.

11 . The airfoil according to claim 10 , wherein the first inflow crossover section comprises a staggered crossover channel and the first outflow crossover section comprises a staggered crossover channel.

12 . The airfoil according to claim 11 , wherein the first inflow crossover section is registered a first distance from an engine central longitudinal axis and the first outflow crossover section is registered a second distance from the engine central longitudinal axis, wherein the first distance and the second distance are different distances.

13 . The airfoil according to claim 1 , wherein the first impingement cavity comprises a plurality of impingement pedestals arranged into a first row and a second row.

14 . The airfoil according to claim 13 , wherein the first row and the second row are registered relative to an engine central longitudinal axis wherein the impingement pedestals of the first row do not align with the impingement pedestals of the second row.

15 . The airfoil according to claim 1 , wherein the first feed cavity further comprises a one-wall pedestal.

16 . An airfoil comprising:
a first feed cavity disposed near a leading edge of the airfoil and defined within a body of the airfoil and configured to receive cooling air; a second feed cavity disposed between the leading edge of the airfoil and a trailing edge of the airfoil and defined within the body of the airfoil and configured to receive cooling air; a first impingement cavity defined within the body of the airfoil and comprising at least one impingement pedestal comprising a one-wall pedestal comprising a boss extending from a surface of the first impingement cavity and into a void defined by a boundary of the first impingement cavity; a second impingement cavity defined within the body of the airfoil and comprising at least one impingement pedestal comprising a one-wall pedestal comprising a boss extending from a surface of the second impingement cavity and into a void defined by a boundary of the second impingement cavity; a third impingement cavity defined within the body of the airfoil and comprising at least one impingement pedestal comprising a one-wall pedestal comprising a boss extending from a surface of the third impingement cavity and into a void defined by a boundary of the third impingement cavity; a first crossover section defined within the body of the airfoil and configured to conduct cooling air from the first feed cavity to the first impingement cavity; a second crossover section defined within the body of the airfoil and configured to conduct cooling air from the second feed cavity to the second impingement cavity; and a third crossover section defined within the body of the airfoil and configured to conduct cooling air from the second feed cavity to the third impingement cavity.

17 . The airfoil according to claim 16 , wherein the airfoil comprises a rotor blade.

18 . The airfoil according to claim 16 , wherein each one-wall pedestal comprises one of zigzag staggering and a round boss.

19 . A method of making an airfoil comprising:
forming a first feed cavity defined within a body of the airfoil and configured to receive cooling air; forming a first impingement cavity defined within the body of the airfoil and comprising a one-wall pedestal; and forming an inflow crossover section defined within the body of the airfoil and configured to conduct cooling air from the first feed cavity to the first impingement cavity, wherein the one-wall pedestal comprises a boss formed to extend from a surface of the first impingement cavity and into a void defined by a boundary of the first impingement cavity.

20 . The method according to claim 19 , wherein the one-wall pedestal comprises a round boss having a height (H) and a diameter (D) defined according to a ratio wherein 0.25<=H/D<=4.0.

Assignees

• United Technologies Corp

Inventors

• Lewis Scott D
• Corcoran Christopher

Classifications

• F05D2260/201

  by impingement of a fluid · CPC title

• F01D5/187 Primary

  Convection cooling · CPC title

• F05D2260/22141

  using fins or ribs · CPC title

• F05D2250/183

  zigzag · CPC title

• F05D2250/14

  elliptical · CPC title