F02K 1/06

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
9989009 Methods and apparatus for sealing variable area fan nozzles of jet enginesOct 31, 12Jun 05, 18The Boeing Company
9926885 Efficient, low pressure ratio propulsor for gas turbine enginesSep 20, 17Mar 27, 18United Technologies Corporation
9909505 Efficient, low pressure ratio propulsor for gas turbine enginesApr 24, 15Mar 06, 18UNITED TECHNOLOGIES CORPORATION
9885313 Gas turbine engine bifurcation located fan variable area nozzleJan 05, 12Feb 06, 18UNITED TECHNOLOGIES CORPORATION
9850776 Variable-section nozzle, and aircraft turbojet engine nacelle equipped with such a nozzleSep 22, 14Dec 26, 17AIRCELLE
9810178 Exhaust nozzle with non-coplanar and/or non-axisymmetric shapeAug 05, 15Nov 07, 17GENERAL ELECTRIC COMPANY
9803585 Axially translating and radially tilting fan nozzle segments with combined actuation and position sensingDec 21, 16Oct 31, 17Not available
9790892 Engine thrust reverser lockJun 12, 15Oct 17, 17WOODWARD HRT, INC.
9776726 Gas turbine cowlDec 09, 14Oct 03, 17ROLLS-ROYCE PLC
9771896 Mixing device and turbofan engine having such mixing deviceApr 03, 14Sep 26, 17MTU AERO ENGINES AG
9732700 Methods and apparatus for passive thrust vectoring and plume deflectionSep 25, 14Aug 15, 17THE BOEING COMPANY
9631577 Threaded rod for system for deploying a deployable divergent segment of a thrusterNov 14, 13Apr 25, 17ARIANEGROUP SAS
9587583 Turbojet engine nacelle having a variable nozzleFeb 05, 14Mar 07, 17AIRCELLE
9581109 Axially translating and radially tilting fan nozzle segments with combined actuation and position sensingApr 11, 14Feb 28, 17Not available
9551294 Sliding nozzle flap assemblyJan 15, 14Jan 24, 17UNITED TECHNOLOGIES CORPORATION
9546618 Methods and apparatus for passive thrust vectoring and plume deflectionOct 24, 13Jan 17, 17THE BOEING COMPANY
9541028 Managing low pressure turbine maximum speed in a turbofan engineOct 12, 06Jan 10, 17UNITED TECHNOLOGIES CORPORATION
9518533 Device and method for assembling a fixed thrust reverser structure of an aircraft propulsion assemblyDec 12, 14Dec 13, 16SAFRAN NACELLES
9506422 Efficient, low pressure ratio propulsor for gas turbine enginesJul 05, 11Nov 29, 16UNITED TECHNOLOGIES CORPORATION
9488130 Variable area fan nozzle systems with improved drive couplingsOct 17, 13Nov 08, 16HONEYWELL INTERNATIONAL INC.

Showing 1 to 20 of 65 results