Invention Grant
- Patent Title: Gas turbine engine having controllable inlet guide vanes
- Patent Title (中): 燃气涡轮发动机具有可控制的入口导叶
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Application No.: US12127104Application Date: 2008-05-27
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Publication No.: US08348600B2Publication Date: 2013-01-08
- Inventor: James W. Norris , Anton G. Banks
- Applicant: James W. Norris , Anton G. Banks
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds PC
- Main IPC: F01D9/04
- IPC: F01D9/04
Abstract:
An inlet guide vane assembly includes an active control feedback system and a plurality of inlet guide vanes. The inlet guide vanes are variable between a plurality of positions. Each of the plurality of inlet guide vanes is positioned in response to an output of the activate control feedback system.
Public/Granted literature
- US20090297334A1 GAS TURBINE ENGINE HAVING CONTROLLABLE INLET GUIDE VANES Public/Granted day:2009-12-03
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