Invention Grant
- Patent Title: Gas turbine engine with fan variable area nozzle to reduce fan instability
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Application No.: US13340787Application Date: 2011-12-30
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Publication No.: US10167813B2Publication Date: 2019-01-01
- Inventor: Gregory A. Kohlenberg , Sean P. Zamora , Frederick M. Schwarz
- Applicant: Gregory A. Kohlenberg , Sean P. Zamora , Frederick M. Schwarz
- 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.
- Main IPC: F02K1/15
- IPC: F02K1/15 ; B64D33/04 ; F02K1/30 ; F02K1/72 ; F01D17/10 ; F01D17/14 ; F01D25/24 ; F02C3/04 ; F02C7/36 ; F02K3/02
Abstract:
A nacelle assembly for a high-bypass gas turbine engine includes a fan variable area nozzle movable relative a fan nacelle to vary a fan nozzle exit area to reduce a fan instability.
Public/Granted literature
- US20160053717A9 GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE TO REDUCE FAN INSTABILITY Public/Granted day:2016-02-25
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