TREA

of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on a substantially axially movable structure

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Industry

  • CPC
  • F02K1/1238
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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

F02K1/1238of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on a substantially axially movable structure
Industries

Patents Grantslast 30 patents

  • 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

    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

    3081596
    • Patent number 3,081,596
    • Issue date Mar 19, 1963
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    2974477
    • Patent number 2,974,477
    • Issue date Mar 14, 1961
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    2969641
    • Patent number 2,969,641
    • Issue date Jan 31, 1961
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    2931169
    • Patent number 2,931,169
    • Issue date Apr 5, 1960
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    2870600
    • Patent number 2,870,600
    • Issue date Jan 27, 1959
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    2846844
    • Patent number 2,846,844
    • Issue date Aug 12, 1958
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents