Invention Grant
- Patent Title: Gas turbine engine airfoil trailing edge passage and core for making same
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Application No.: US14390496Application Date: 2013-03-12
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Publication No.: US09938837B2Publication Date: 2018-04-10
- Inventor: Jeffrey R. Levine , Jeffrey S. Beattie , Malcolm C. Staddon
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- International Application: PCT/US2013/030332 WO 20130312
- International Announcement: WO2013/180792 WO 20131205
- Main IPC: F01D5/18
- IPC: F01D5/18 ; B22C9/10

Abstract:
An airfoil has a body that includes leading and trailing edges that adjoin pressure and suction sides to provide an exterior airfoil surface. A cooling passage extends in a radial direction from a root to a tip. A trailing edge cooling passage interconnects the cooling passage to the trailing edge. The trailing edge cooling passage includes first and second pedestals of different sizes that are arranged in a repeating pattern with respect to pedestals of the same size and with respect to pedestals of different sizes.
Public/Granted literature
- US20150118064A1 GAS TURBINE ENGINE AIRFOIL TRAILING EDGE PASSAGE AND CORE FOR MAKING SAME Public/Granted day:2015-04-30
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