Invention Grant
- Patent Title: Airfoil contour for low-loss on-boarding of cooling air through an articulating spindle
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Application No.: US15034951Application Date: 2014-11-03
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Publication No.: US10385728B2Publication Date: 2019-08-20
- Inventor: Thomas N. Slavens , Eric A. Grover , John D. Teixeira
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- International Application: PCT/US2014/063652 WO 20141103
- International Announcement: WO2015/073242 WO 20150521
- Main IPC: F01D25/12
- IPC: F01D25/12 ; F01D17/16 ; F01D5/14 ; F01D9/04 ; F01D9/06 ; F01D5/02 ; F01D5/12 ; F01D17/14 ; F02C3/04

Abstract:
A turbine stator vane assembly for a gas turbine engine is disclosed and includes an airfoil rotatable about an axis transverse to an engine longitudinal axis. The airfoil includes outer walls defining an inner chamber between a pressure side and a suction side of the airfoil. At least one spindle supports rotation of the airfoil and includes a feed opening for communicating cooling air into the inner chamber. An inlet defines a passage between the feed opening and the inner chamber and includes a protrusion of the outer wall on at least one of the pressure side and suction side of the airfoil.
Public/Granted literature
- US20160290158A1 AIRFOIL CONTOUR FOR LOW-LOSS ON-BOARDING OF COOLING AIR THROUGH AN ARTICULATING SPINDLE Public/Granted day:2016-10-06
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