Invention Grant
- Patent Title: Vane assembly for a gas turbine engine
- Patent Title (中): 燃气轮机的叶片组件
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Application No.: US13196980Application Date: 2011-08-03
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Publication No.: US09279335B2Publication Date: 2016-03-08
- Inventor: Tracy A. Propheter-Hinckley
- Applicant: Tracy A. Propheter-Hinckley
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds
- Main IPC: F01D9/04
- IPC: F01D9/04 ; F01D17/16

Abstract:
A vane assembly for a gas turbine engine includes a first platform, a second platform, and an airfoil that extends radially across an annulus between the first platform and the second platform. The airfoil is centered relative to a centerline axis of the second platform and is offset relative to a centerline axis of the first platform.
Public/Granted literature
- US20130034435A1 VANE ASSEMBLY FOR A GAS TURBINE ENGINE Public/Granted day:2013-02-07
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