Invention Grant
- Patent Title: Turbine engine with a platform cooling circuit
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Application No.: US15481628Application Date: 2017-04-07
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Publication No.: US10508548B2Publication Date: 2019-12-17
- Inventor: James Michael Hoffman , Weston Nolan Dooley , Aaron Ezekiel Smith , Steven Robert Brassfield
- 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 ; F01D5/08

Abstract:
An airfoil assembly for a turbine engine can comprise a platform having first and second opposing surfaces, an airfoil extending from the first surface, a base extending from the second surface, and a platform cooling circuit including a feed tube, a first branch, a second branch, and a flow divider.
Public/Granted literature
- US20180291742A1 TURBINE ENGINE WITH A PLATFORM COOLING CIRCUIT Public/Granted day:2018-10-11
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