TREA

of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, the internal downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series and at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantial...

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  • CPC
  • F02K1/1292
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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

F02K1/1292of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, the internal downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series and at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantial...
Industries

Patents Grantslast 30 patents

  • Information Patent Grant

    Convergent-divergent flap pair for a variable-geometry turbojet eng...
    • Patent number 11,713,730
    • Issue date Aug 1, 2023
    • SAFRAN AIRCRAFT ENGINES
    • Thierry Kohn
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Secondary nozzle for jet engine
    • Patent number 10,400,710
    • Issue date Sep 3, 2019
    • General Electric Company
    • David Lynn Dawson
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Gas turbine engine including a third flowpath exhaust nozzle
    • Patent number 10,197,008
    • Issue date Feb 5, 2019
    • United Technologies Corporation
    • Gary D. Roberge
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Enhanced durability drive link for high load misalignment
    • Patent number 10,100,779
    • Issue date Oct 16, 2018
    • United Technologies Corporation
    • Hannes A. Alholm
    • B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • Information Patent Grant

    Stepped fairing modulated exhaust cooling
    • Patent number 10,087,884
    • Issue date Oct 2, 2018
    • United Technologies Corporation
    • Donald W. Peters
    • 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

    Nozzle with an adjustable throat
    • Patent number 8,769,959
    • Issue date Jul 8, 2014
    • Rolls-Royce Corporation
    • Von David Baker
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Nozzle with an adjustable throat
    • Patent number 7,793,504
    • Issue date Sep 14, 2010
    • Rolls-Royce Corporation
    • Von David Baker
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Purged flameholder fuel shield
    • Patent number 7,581,398
    • Issue date Sep 1, 2009
    • General Electric Company
    • Jeffrey Carl Mayer
    • F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
  • Information Patent Grant

    Turbine engine nozzle
    • Patent number 7,546,738
    • Issue date Jun 16, 2009
    • United Technologies Corporation
    • Donald W. Peters
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Grant

    Device for reducing jet engine exhaust noise using oscillating jets
    • Patent number 7,308,966
    • Issue date Dec 18, 2007
    • General Electric Company
    • Anurag Gupta
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Turbine engine nozzle
    • Patent number 7,225,622
    • Issue date Jun 5, 2007
    • United Technologies Corporation
    • Dale W. Petty
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Axial divergent section slot nozzle
    • Patent number 7,096,661
    • Issue date Aug 29, 2006
    • United Technologies Corporation
    • Robert H. Bush
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Turbine engine nozzle
    • Patent number 7,007,483
    • Issue date Mar 7, 2006
    • United Technologies Corporation
    • Donald W. Peters
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Ejector cooled nozzle
    • Patent number 6,983,602
    • Issue date Jan 10, 2006
    • General Electric Company
    • Darrell Glenn Senile
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Turbine engine nozzle
    • Patent number 6,871,797
    • Issue date Mar 29, 2005
    • United Technologies Corporation
    • Donald W. Peters
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    System for activating an adjustable tube by means of an elastic rin...
    • Patent number 6,378,294
    • Issue date Apr 30, 2002
    • Societe Nationale d'Etude et de Construction de Moteurs d'Aviation - S.N.E.C....
    • François Abbe
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Swiveling, converging-diverging, axisymmetric exhaust nozzle
    • Patent number 6,375,095
    • Issue date Apr 23, 2002
    • Societe Nationale d'Etude et de Construction de Moteurs d'Aviation - S.N.E.C....
    • Didier Georges Feder
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Axisymmetric, converging-diverging exhaust nozzle swiveled by a gui...
    • Patent number 6,360,527
    • Issue date Mar 26, 2002
    • SNECMA Moteurs
    • Didier Georges Feder
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Axi-nozzle ejector seal
    • Patent number 6,347,510
    • Issue date Feb 19, 2002
    • United Technologies Corporation
    • Timothy J. McAlice
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Universal-joint vectoring system for a turbojet-engine exhaust nozzle
    • Patent number 6,327,846
    • Issue date Dec 11, 2001
    • SCNEMA Moteurs
    • Didier Georges Feder
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Axisymmetric, directable and adjustable turbojet-engine exhaust nozzle
    • Patent number 6,276,126
    • Issue date Aug 21, 2001
    • Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (S.N.E.C.M...
    • Philippe Pierre Vincent Bouiller
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Hybrid-composite gas turbine exhaust nozzle compression link
    • Patent number 6,240,720
    • Issue date Jun 5, 2001
    • General Electric Company
    • Wu-Yang Tseng
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Vectoring nozzle control system
    • Patent number 6,195,981
    • Issue date Mar 6, 2001
    • General Electric Company
    • Charles F. Hanley
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Variable geometry turbojet engine exhaust nozzle
    • Patent number 5,934,564
    • Issue date Aug 10, 1999
    • Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
    • Philippe Pierre Vincent Bouiller
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Axisymmetric vectoring nozzle
    • Patent number 5,511,376
    • Issue date Apr 30, 1996
    • United Technologies Corporation
    • William K. Barcza
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Variable geometry turbojet engine exhaust nozzle
    • Patent number 5,494,221
    • Issue date Feb 27, 1996
    • Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
    • Fabrice M. O. Cot
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Axisymmetric vectoring exhaust nozzle thermal shield
    • Patent number 5,485,959
    • Issue date Jan 23, 1996
    • General Electric Company
    • Jonathan M. Wood
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Cooling system for a divergent section of a nozzle
    • Patent number 5,484,105
    • Issue date Jan 16, 1996
    • General Electric Company
    • Robert M. Ausdenmoore
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Divergent slave petal for sealing in variable geometry exhaust nozz...
    • Patent number 5,461,856
    • Issue date Oct 31, 1995
    • Sener, Ingenieria y Sistemas, S.A.
    • Jose I. I. Mendia
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

  • Information Patent Application

    CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENG...
    • Publication number 20220290631
    • Publication date Sep 15, 2022
    • SAFRAN AIRCRAFT ENGINES
    • Thierry KOHN
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    ENHANCED DURABILITY DRIVE LINK FOR HIGH LOAD MISALIGNMENT
    • Publication number 20170292472
    • Publication date Oct 12, 2017
    • United Technologies Corporation
    • HANNES A. ALHOLM
    • B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • Information Patent Application

    SECONDARY NOZZLE FOR JET ENGINE
    • Publication number 20140345254
    • Publication date Nov 27, 2014
    • GENERAL ELECTRIC COMPANY
    • David Lynn DAWSON
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    NOZZLE WITH AN ADJUSTABLE THROAT
    • Publication number 20100327078
    • Publication date Dec 30, 2010
    • Von David Baker
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    PURGED FLAMEHOLDER FUEL SHIELD
    • Publication number 20090113894
    • Publication date May 7, 2009
    • General Electric Company
    • Jeffrey Carl Mayer
    • F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
  • Information Patent Application

    Nozzle with an adjustable throat
    • Publication number 20070256419
    • Publication date Nov 8, 2007
    • Rolls-Royce Corporation
    • Von David Baker
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    Turbine engine nozzle
    • Publication number 20070062199
    • Publication date Mar 22, 2007
    • United Technologies Corporation
    • Curtis C. Cowan
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Application

    TURBINE ENGINE NOZZLE
    • Publication number 20070039328
    • Publication date Feb 22, 2007
    • Dale W. Petty
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    Turbine engine nozzle
    • Publication number 20060144036
    • Publication date Jul 6, 2006
    • United Technologies Corporation
    • Donald W. Peters
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Application

    EJECTOR COOLED NOZZLE
    • Publication number 20050235628
    • Publication date Oct 27, 2005
    • Darrell Glenn Senile
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    Turbine engine nozzle
    • Publication number 20050217271
    • Publication date Oct 6, 2005
    • Donald W. Peters
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    Axial divergent section slot nozzle
    • Publication number 20050210861
    • Publication date Sep 29, 2005
    • Robert H. Bush
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    Device for reducing jet engine exhaust noise using oscillating jets
    • Publication number 20050144935
    • Publication date Jul 7, 2005
    • General Electric Company
    • Anurag Gupta
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    TURBINE ENGINE NOZZLE
    • Publication number 20050011195
    • Publication date Jan 20, 2005
    • Donald W. Peters
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS