Invention Grant
- Patent Title: Gas turbine engine airfoil with auxiliary flow channel
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Application No.: US15029802Application Date: 2014-10-07
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Publication No.: US10280757B2Publication Date: 2019-05-07
- Inventor: Daniel Bernard Kupratis , Frederick M. Schwarz
- 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/US2014/059394 WO 20141007
- International Announcement: WO2015/065659 WO 20150507
- Main IPC: F01D5/14
- IPC: F01D5/14 ; F01D17/16 ; F01D9/04 ; F01D17/14 ; F04D29/68 ; F04D29/56
Abstract:
A component for a gas turbine engine, according to an exemplary aspect of the present disclosure includes, among other things, an airfoil that includes a pressure side surface and a suction side surface that join together at a leading edge and a trailing edge and a flow channel that extends between the pressure side surface and the suction side surface.
Public/Granted literature
- US20160245091A1 GAS TURBINE ENGINE AIRFOIL WITH AUXILIARY FLOW CHANNEL Public/Granted day:2016-08-25
Information query
