Invention Grant
- Patent Title: Engine component with porous trench
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Application No.: US15238150Application Date: 2016-08-16
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Publication No.: US10508551B2Publication Date: 2019-12-17
- Inventor: Ronald Scott Bunker
- 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: F01D5/18
- IPC: F01D5/18 ; F01D5/28 ; F01D9/04 ; F01D25/12 ; F02K3/06 ; F04D29/32 ; F04D29/54 ; F04D29/58 ; F01D9/06

Abstract:
An apparatus and method for cooling an engine component, such as an airfoil, including a wall to separate a hot flow from a cooling fluid flow. The component can include at least one trench disposed in a hot surface. The trench can be fed with the cooling fluid flow to cool the engine component along the hot surface with the cooling fluid flow.
Public/Granted literature
- US20180051565A1 ENGINE COMPONENT WITH POROUS TRENCH Public/Granted day:2018-02-22
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