Invention Grant
- Patent Title: Gas turbine engine airfoil
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Application No.: US15115779Application Date: 2015-02-12
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Publication No.: US10352331B2Publication Date: 2019-07-16
- Inventor: Edward J. Gallagher , Lisa I. Brilliant , Joseph C. Straccia , Stanley J. Balamucki , Mark A. Stephens , Kate Hudon
- 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/US2015/015579 WO 20150212
- International Announcement: WO2015/175044 WO 20151119
- Main IPC: F02C3/04
- IPC: F02C3/04 ; F04D29/32 ; F01D5/14 ; F04D29/54 ; F02C3/06 ; F02C7/36 ; F02K3/06 ; F04D29/38
Abstract:
An airfoil of a turbine engine includes pressure and suction sides and extends in a radial direction from a 0% span position to a 100% span position. The airfoil has a relationship between a camber angle and span position that defines a curve with the camber angle having a positive slope from 0% span to 100% span.
Public/Granted literature
- US20170167503A1 GAS TURBINE ENGINE AIRFOIL Public/Granted day:2017-06-15
Information query
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