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US 2014/0208771 A1Published application
Gas turbine engine component cooling arrangement
AssigneeUnited Technologies Corporation
InventorsJames M. Koonankeil, Edward F. Pietraszkiewicz, Dominic J. Mongillo, Jr.
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Abstract
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a body portion having an exterior surface and an internal surface. A cavity is disposed inside of the body portion. A cooling hole extends between the exterior surface and the internal surface and includes a metering section having an outlet and an inlet. The inlet is shaped dissimilar to the outlet.
Claims20
A component for a gas turbine engine, comprising:
- a body portion having an exterior surface and an internal surface;
- a cavity disposed inside of said body portion;
- and
- a cooling hole that extends between said exterior surface and said internal surface and includes a metering section having an outlet and an inlet, wherein said inlet is shaped dissimilar to said outlet.
1 more element
A gas turbine engine, comprising:
- a compressor section;
- a combustor section in fluid communication with said compressor section;
- a turbine section in fluid communication said combustor section;
- and
- a component disposed in at least one of said compressor section and said turbine section, wherein said component includes:
- a body portion having an exterior surface and an internal surface;
- a cavity disposed inside said body portion;
- and
- a cooling hole that extends between said exterior surface and said internal surface and includes a metering section having an outlet and an inlet, wherein said inlet is shaped dissimilar to said outlet.
6 more elements
Dependencies are inferred from the claim text.