Invention Grant
- Patent Title: Engine component with cooling hole
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Application No.: US16733377Application Date: 2020-01-03
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Publication No.: US11131213B2Publication Date: 2021-09-28
- Inventor: Kelli Marie Fishback , Jonathan Russell Ratzlaff , Steven Robert Brassfield , Kurt Thomas Whittington
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: McGarry Bair PC
- Main IPC: F01D5/12
- IPC: F01D5/12 ; F01D25/12

Abstract:
An airfoil assembly for a turbine engine that includes a platform, a dovetail, an airfoil. The airfoil assembly can further include a cooling air circuit that fluidly connects to a platform cooling passage. The cooling air circuit and platform cooling passage can be contained within or housed at least in part by the platform, the dovetail, or the airfoil. The cooling air circuit can also include a deflector.
Public/Granted literature
- US20210207493A1 ENGINE COMPONENT WITH COOLING HOLE Public/Granted day:2021-07-08
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