Film hole with protruding flow accumulator

Patent metadata

Field	Value
Publication number	US-9957810-B2
Application number	US-201514852896-A
Country	US
Kind code	B2
Filing date	Sep 14, 2015
Priority date	Oct 20, 2014
Publication date	May 1, 2018
Grant date	May 1, 2018

Abstract

A wall of a gas turbine engine is provided. The wall may comprise an external surface adjacent a gas path and an internal surface adjacent an internal flow path. A film hole may have an inlet at the internal surface and an outlet at the external surface. A flow accumulator adjacent the inlet may protrude from the internal surface. A method of making an engine component is also provided and comprises the step of forming a component wall comprising an accumulator on an internal surface and a film hole defined by the component wall. The film hole may include an opening adjacent the accumulator and defined by the internal surface.

First claim

What is claimed is:

1. A gas turbine engine component, comprising:
an internal flow path defined by an internal surface and extending from an upstream direction to a downstream direction;
a component wall including a film hole comprising:
an inlet defined by the internal surface,
an outlet defined by an external surface, wherein the film hole extends from the inlet at least partially in the upstream direction,

a flow accumulator extending from the component wall adjacent the inlet, wherein the flow accumulator is configured to direct fluid into the inlet, through the film hole, and through the outlet, wherein the flow accumulator is at least partially defined by a first surface extending from a sidewall of the film hole in the upstream direction, wherein the first surface is spaced from, faces, and at least partially overlaps the inlet in the upstream direction.

2. The gas turbine engine component of claim 1 , wherein the flow accumulator comprises a shape configured to turbulate an air flow.

3. The gas turbine engine component of claim 1 , further comprising:
a meter of the film hole comprising a hydraulic diameter; and
a height of the flow accumulator, wherein a ratio of the height over the hydraulic diameter is less than or equal to 10.

4. The gas turbine engine component of claim 1 , wherein the film hole comprises a diffuser in fluid communication with the flow accumulator.

5. The gas turbine engine component of claim 1 , wherein the flow accumulator overhangs the inlet.

6. The gas turbine engine component of claim 1 , wherein the flow accumulator is configured to increase a velocity of a coolant through the film hole by conditioning a flow of the coolant adjacent to the inlet.

7. A gas turbine engine part, comprising:
an internal flow path defined by an internal surface and extending from an upstream direction to a downstream direction;
an external surface defining an outlet;
an internal surface opposite the external surface and defining an inlet;
a film hole extending from the inlet to the outlet at least partially in the upstream direction; and
a flow accumulator protruding from the internal surface and partially bounding the film hole, wherein the flow accumulator is at least partially defined by a first surface extending from a sidewall of the film hole in the upstream direction, wherein the first surface is spaced from, faces, and at least partially overlaps the inlet in the upstream direction.

8. The gas turbine engine part of claim 7 , wherein the flow accumulator is in fluid communication with the film hole.

9. The gas turbine engine part of claim 7 , wherein the film hole further comprises a diffuser in fluid communication with the flow accumulator.

10. The gas turbine engine part of claim 7 , further comprising:
a meter of the film hole comprising a hydraulic diameter; and
a height of the flow accumulator, wherein a ratio of the height over the hydraulic diameter is less than or equal to 10.

11. The gas turbine engine part of claim 7 , wherein the flow accumulator overhangs the inlet of the film hole.

12. A method of making an engine component, comprising:
forming a component comprising an accumulator on an internal surface and a film hole aligned with the accumulator, the film hole comprising an opening adjacent the accumulator and defined by the internal surface, wherein the accumulator is configured to direct fluid into the opening, wherein the accumulator is at least partially defined by a first surface extending from a sidewall of the film hole in the upstream direction, wherein the first surface is spaced from, faces, and at least partially overlaps the opening in the upstream direction.

13. The method of claim 12 , wherein the forming the component wall further comprises additively manufacturing the component wall.

14. The method of claim 12 , further forming the component wall by at least one of direct metal laser sintering, selective laser sintering, selective laser melting, electron-beam melting, or electron-beam freeform fabrication.

15. The method of claim 12 , wherein the forming the component wall further comprises:
forming a core of the component wall using additive manufacturing; and
casting the component wall using the core.

16. The method of claim 15 , further comprising forming a mold as one piece with the core using additive manufacturing.

Assignees

• United Technologies Corp

Inventors

• Musto Clifford J
• Loricco Nicholas M
• Slavens Thomas N
• Jennings Timothy J
• Clum Carey
• Moore Sasha M
• Mcbrien John
• Quach San
• Whitfield Christopher

Classifications

• F05D2230/22

  by sintering · CPC title

• F05D2230/21

  by casting · CPC title

• F05D2230/31

  Layer deposition · CPC title

• B22C9/10

  Cores; Manufacture or installation of cores {(breaker cores B22C9/084)} · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title