Gas turbine engine components with lateral and forward sweep film cooling holes

Patent metadata

Field	Value
Publication number	US-10113433-B2
Application number	US-201213644824-A
Country	US
Kind code	B2
Filing date	Oct 4, 2012
Priority date	Oct 4, 2012
Publication date	Oct 30, 2018
Grant date	Oct 30, 2018

Abstract

An engine component includes a body having an internal surface and an external surface, the internal surface at least partially defining an internal cooling circuit. The engine component further includes a plurality of cooling holes formed in the body and extending between the internal cooling circuit and the external surface of the body. The plurality of cooling holes includes a first cooling hole with forward diffusion and lateral diffusion.

First claim

What is claimed is:

1. An engine component, comprising:
a body having an internal surface and an external surface, the internal surface at least partially defining an internal cooling circuit; and
a plurality of cooling holes formed in the body and extending between the internal cooling circuit and the external surface of the body, the plurality of cooling holes including a first cooling hole with forward diffusion and lateral diffusion,
wherein the first cooling hole includes an inlet at the internal cooling circuit, a metering section extending from the inlet, a first exit portion extending from the metering section, a second exit portion extending from the first exit portion, and an outlet defined on the external surface and fluidly coupled to the second exit portion, wherein the metering section is an oval-shaped cylinder,
wherein the first exit portion extends at a first angle relative to the metering section and the second exit portion extends at a second angle relative to the metering section, the second angle being greater than the first angle to provide the forward diffusion,
wherein the outlet is a multi-lobe shape formed by a first oval, a second oval, and a third oval, each oval having a first end and a second end, wherein the first ends of the first oval, the second oval, and the third oval at least partially overlap, and wherein the second ends of the first oval, the second oval, and the third ovals are splayed relative to one another to provide the lateral diffusion.

2. The engine component of claim 1 , wherein the first oval extends relative to a first side of the second oval at a third angle, and the third oval extends relative to a second side of the second oval at a fourth angle, and wherein the first oval has a first length, the second oval has a second length, and the third oval has a third length.

3. The engine component of claim 2 , wherein the third angle is equal to the fourth angle.

4. The engine component of claim 2 , wherein the first length and the third length are approximately equal.

5. The engine component of claim 4 , wherein the second length and the first length are approximately equal.

6. The engine component of claim 4 , wherein the second length is greater than the first length.

7. The engine component of claim 2 , wherein the third angle is different than the fourth angle.

8. The engine component of claim 2 , wherein the second length is greater than the first length.

9. The engine component of claim 2 , wherein the internal cooling circuit includes an internal passage within the body between the internal surface and the external surface, and wherein the second exit portion of the first cooling hole at the second angle places a downstream edge of the first cooling hole on a portion of the external surface adjacent to the internal passage.

10. An engine component, comprising:
a body having an internal surface and an external surface, the internal surface at least partially defining an internal cooling circuit; and
a plurality of cooling holes formed in the body and extending between the internal cooling circuit and the external surface of the body, the plurality of cooling holes including a first cooling hole with double forward diffusion and double lateral diffusion,
wherein the first cooling hole includes an inlet at the internal cooling circuit, a metering section extending from the inlet, a first exit portion extending from the metering section, a second exit portion extending from the first exit portion, and an outlet defined on the external surface and fluidly coupled to the second exit portion, wherein the metering section is an oval-shaped cylinder,
wherein the first exit portion is curved with a first radius of curvature and the second exit portion is curved with a second radius of curvature, the second radius of curvature being greater than the first radius of curvature to provide the double forward diffusion,
wherein the outlet is defined by a leading edge, a trailing edge, and first and second sides extending between the leading edge and the trailing edge, wherein the first side has leading portion extending from the leading edge at a first angle relative to a longitudinal surface axis and a trailing portion extending from the leading portion at a second angle relative to the longitudinal surface axis, the second angle being greater than the first angle to provide the double lateral diffusion.

11. The engine component of claim 10 , wherein the first and second sides are asymmetric relative to one another.

12. An engine component, comprising:
a body having an internal surface and an external surface, the internal surface at least partially defining an internal cooling circuit; and
a plurality of cooling holes formed in the body and extending between the internal cooling circuit and the external surface of the body, the plurality of cooling holes including a first cooling hole with double forward diffusion and double lateral diffusion,
wherein the first cooling hole includes an inlet at the internal cooling circuit, a metering section extending from the inlet, a first exit portion extending from the metering section, a second exit portion extending from the first exit portion, and an outlet defined on the external surface and fluidly coupled to the second exit portion, wherein the metering section is an oval-shaped cylinder,
wherein the first exit portion is curved with a first radius of curvature and the second exit portion is curved with a second radius of curvature, the second radius of curvature being greater than the first radius of curvature to provide the double forward diffusion,
wherein the outlet is defined by a leading edge, a trailing edge, and first and second sides extending between the leading edge and the trailing edge, wherein the first side has leading portion extending from the leading edge at a first angle relative to a longitudinal surface axis and a trailing portion extending from the leading portion at a second angle relative to the longitudinal surface axis, the second angle being greater than the first angle to provide the double lateral diffusion, and
wherein the first angle is approximately 10°-12° and the second angle is approximately 13°-15°.

Assignees

• Honeywell Int Inc

Inventors

• Morris Mark C
• Waldman David
• Malak Malak Fouad
• Tapia Luis

Classifications

• F05D2250/324

  divergent · CPC title

• F01D5/186 Primary

  Film cooling (F01D5/187 takes precedence) · CPC title

• F05D2250/71

  curved · CPC title

• F05D2260/202

  by film cooling · CPC title

• Y02T50/676

  Cross-Sectional Technologies · mapped topic