TREA

of two series of flaps, both having their flaps hinged at their upstream ends on a fixed structure

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  • F02K1/123
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Parent Industries

FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F02Combustion engines F02KJET-PROPULSION PLANTS F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle Jet pipes or nozzles peculiar thereto

Current Industry

F02K1/123of two series of flaps, both having their flaps hinged at their upstream ends on a fixed structure
Industries

Patents Grantslast 30 patents

  • Information Patent Grant

    Aircraft propulsion system exhaust nozzle with ejector passage(s)
    • Patent number 11,754,018
    • Issue date Sep 12, 2023
    • Rohr, Inc.
    • Timothy Gormley
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Variable area nozzle and method for operating same
    • Patent number 11,713,731
    • Issue date Aug 1, 2023
    • Rohr, Inc.
    • Timothy Gormley
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    2D variable-area plug nozzle
    • Patent number 11,661,905
    • Issue date May 30, 2023
    • Florida Turbine Technologies, Inc.
    • Robert A. Ress
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Thrust reverser for variable area nozzle
    • Patent number 11,566,584
    • Issue date Jan 31, 2023
    • Rohr, Inc.
    • Timothy Gormley
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Nozzle with variable throat and exit areas
    • Patent number 10,662,896
    • Issue date May 26, 2020
    • Rolls-Royce PLC
    • Jonathan V Watson
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Nozzle for jet engines
    • Patent number 10,378,477
    • Issue date Aug 13, 2019
    • Rolls-Royce North American Technologies Inc.
    • Kenneth M. Pesyna
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Variable-section nozzle, and aircraft turbojet engine nacelle equip...
    • Patent number 9,850,776
    • Issue date Dec 26, 2017
    • Aircelle
    • Hervé Hurlin
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Three stream, variable area, vectorable nozzle
    • Patent number 9,845,768
    • Issue date Dec 19, 2017
    • Rolls-Royce North American Technologies, Inc.
    • Kenneth M. Pesyna
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Three stream, variable area fixed aperture nozzle with pneumatic ac...
    • Patent number 9,677,501
    • Issue date Jun 13, 2017
    • Rolls-Royce North American Technologies, Inc.
    • Anthony F. Pierluissi
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Compact actuation system for flow nozzle
    • Patent number 9,464,594
    • Issue date Oct 11, 2016
    • Rolls-Royce North America Technologies, Inc.
    • Kenneth M. Pesyna
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Variable jet engine outlet with a mainly circle sector-formed cross...
    • Patent number 9,341,141
    • Issue date May 17, 2016
    • Saab AB
    • Jakob Bjerkemo
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Grant

    Nacelle for an aircraft bypass turbojet engine
    • Patent number 9,243,587
    • Issue date Jan 26, 2016
    • Aircelle
    • Herve Hurlin
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Gas turbine engine with fan variable area nozzle, nacelle assembly...
    • Patent number 8,365,515
    • Issue date Feb 5, 2013
    • United Technologies Corporation
    • Edward F. Migliaro
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Shape changing structure
    • Patent number 7,216,831
    • Issue date May 15, 2007
    • The Boeing Company
    • Jeffrey H Wood
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Methods and apparatus for flade engine nozzle
    • Patent number 6,948,317
    • Issue date Sep 27, 2005
    • General Electric Company
    • Bernard James Renggli
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Grant

    Actuating system for a variable area exhaust nozzle
    • Patent number 5,611,489
    • Issue date Mar 18, 1997
    • Societe Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
    • Yves R. J. Berneuil
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Combination turbojet engine nozzle and thrust reverser
    • Patent number 5,470,020
    • Issue date Nov 28, 1995
    • Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
    • Pascal N. Brossier
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Eccentric flap nozzle
    • Patent number 5,081,835
    • Issue date Jan 21, 1992
    • United Technologies Corporation
    • Joseph H. Ewing
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Two dimensional nozzle for a turbojet engine
    • Patent number 4,955,541
    • Issue date Sep 11, 1990
    • Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
    • Olivier Carteron
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Yaw and pitch convergent-divergent thrust vectoring nozzle
    • Patent number 4,836,451
    • Issue date Jun 6, 1989
    • United Technologies Corporation
    • Paul W. Herrick
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Exhaust nozzle assembly for a turbojet engine
    • Patent number 4,641,783
    • Issue date Feb 10, 1987
    • Societe Nationale d'Etude et de Construction de Meteur d'Aviation (SNECMA)
    • Andre A. M. L. Camboulives
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Flap-type nozzle with built-in reverser
    • Patent number 4,382,551
    • Issue date May 10, 1983
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    3814323
    • Patent number 3,814,323
    • Issue date Jun 4, 1974
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    3598319
    • Patent number 3,598,319
    • Issue date Aug 10, 1971
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    3570769
    • Patent number 3,570,769
    • Issue date Mar 16, 1971
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    3537647
    • Patent number 3,537,647
    • Issue date Nov 3, 1970
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    3527409
    • Patent number 3,527,409
    • Issue date Sep 8, 1970
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    3511441
    • Patent number 3,511,441
    • Issue date May 12, 1970
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    3463402
    • Patent number 3,463,402
    • Issue date Aug 26, 1969
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    3439504
    • Patent number 3,439,504
    • Issue date Apr 22, 1969
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

  • Information Patent Application

    VARIABLE AREA NOZZLE AND METHOD FOR OPERATING SAME
    • Publication number 20230213002
    • Publication date Jul 6, 2023
    • Rohr, Inc.
    • Timothy Gormley
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    AIRCRAFT NOZZLE
    • Publication number 20200025129
    • Publication date Jan 23, 2020
    • Rolls-Royce plc
    • Jack F. COLEBROOKE
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    AIRCRAFT NOZZLE
    • Publication number 20190226423
    • Publication date Jul 25, 2019
    • Rolls-Royce plc
    • Jack F. COLEBROOKE
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    AIRCRAFT NOZZLE
    • Publication number 20190226424
    • Publication date Jul 25, 2019
    • Rolls-Royce plc
    • Jack F COLEBROOKE
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    NOZZLE
    • Publication number 20180171931
    • Publication date Jun 21, 2018
    • Rolls-Royce plc
    • Jonathan V. WATSON
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    HYBRID EXHAUST NOZZLE
    • Publication number 20170145955
    • Publication date May 25, 2017
    • Rolls-Royce North American Technologies, Inc.
    • Von D. Baker
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    COMPACT ACTUATION SYSTEM FOR FLOW NOZZLE
    • Publication number 20150129676
    • Publication date May 14, 2015
    • Rolls-Royce North American Technologies, Inc.
    • Kenneth M. Pesyna
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    PASSIVE TANGENTIAL EJECTOR FOR AN EXHAUST NOZZLE OF A GAS TURBINE E...
    • Publication number 20150122905
    • Publication date May 7, 2015
    • United Technologies Corporation
    • Keegan M. Martin
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    THREE STREAM, VARIABLE AREA FIXED APERTURE NOZZLE WITH PNEUMATIC AC...
    • Publication number 20140263737
    • Publication date Sep 18, 2014
    • Rolls-Royce North American Technologies, Inc.
    • Anthony F. Pierluissi
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    VARIABLE JET ENGINE OUTLET WITH A MAINLY CIRCLE SECTOR-FORMED CROSS...
    • Publication number 20140103141
    • Publication date Apr 17, 2014
    • SAAB AB
    • Jakob Bjerkemo
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE
    • Publication number 20130230391
    • Publication date Sep 5, 2013
    • Aircelle
    • Herve Hurlin
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE, NACELLE ASSEMBLY...
    • Publication number 20100139243
    • Publication date Jun 10, 2010
    • Edward F. Migliaro, JR.
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    Shape changing structure
    • Publication number 20060124801
    • Publication date Jun 15, 2006
    • Jeffrey H. Wood
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    METHODS AND APPARATUS FOR FLADE ENGINE NOZZLE
    • Publication number 20050091982
    • Publication date May 5, 2005
    • Bernard James Renggli
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...