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 the downstream ends of the flaps of the upstream series

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Industry

  • CPC
  • F02K1/1223
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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

F02K1/1223of 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 the downstream ends of the flaps of the upstream series
Industries

Patents Grantslast 30 patents

Patents Applicationslast 30 patents

  • Information Patent Application

    MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS...
    • Publication number 20250052210
    • Publication date Feb 13, 2025
    • Rohr, Inc.
    • JOHANN STEVEN SCHRELL
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    TURBOJET ENGINE REAR PORTION HAVING AN AUGMENTED A9/A8 NOZZLE AREA...
    • Publication number 20240141852
    • Publication date May 2, 2024
    • SAFRAN AIRCRAFT ENGINES
    • Thierry KOHN
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    TURBOJET ENGINE REAR PART COMPRISING A NOZZLE HAVING FLAPS COMPRISI...
    • Publication number 20240003316
    • Publication date Jan 4, 2024
    • SAFRAN AIRCRAFT ENGINES
    • Thierry KOHN
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS...
    • Publication number 20230272760
    • Publication date Aug 31, 2023
    • Rohr, Inc.
    • JOHANN STEVEN SCHRELL
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS...
    • Publication number 20230160355
    • Publication date May 25, 2023
    • Rohr, Inc.
    • JOHANN STEVEN SCHRELL
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIAT...
    • Publication number 20220364527
    • Publication date Nov 17, 2022
    • Blue Origin, LLC
    • Nathaniel Cantor
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • 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

    CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENG...
    • Publication number 20220275771
    • Publication date Sep 1, 2022
    • SAFRAN AIRCRAFT ENGINES
    • François LEGLAYE
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    EXHAUST NOZZLE
    • Publication number 20210131379
    • Publication date May 6, 2021
    • Rolls-Royce plc
    • Jack F. COLEBROOKE
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    CONVERGENT-DIVERGENT NOZZLE MECHANISM
    • Publication number 20190345894
    • Publication date Nov 14, 2019
    • United Technologies Corporation
    • Brandon T. Slaney
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    ASYMMETRIC LOAD COMPENSATION SYSTEM
    • Publication number 20180238267
    • Publication date Aug 23, 2018
    • HAMILTON SUNDSTRAND CORPORATION
    • Craig T. Stambaugh
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    COMPOSITE WEAR PAD FOR EXHAUST NOZZLE
    • Publication number 20180238268
    • Publication date Aug 23, 2018
    • United Technologies Corporation
    • Donald W. PETERS
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    IMPINGEMENT COOLED NOZZLE LINER
    • Publication number 20180156053
    • Publication date Jun 7, 2018
    • United Technologies Corporation
    • Curtis C. Cowan
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    GAS TURBINE ENGINE CONVERGENT/DIVERGENT EXHAUST NOZZLE DIVERGENT SE...
    • Publication number 20170159607
    • Publication date Jun 8, 2017
    • United Technologies Corporation
    • Truc Luong
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    DIVERGENT FLAP
    • Publication number 20160237948
    • Publication date Aug 18, 2016
    • United Technologies Corporation
    • Meggan Harris
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    STEPPED FAIRING MODULATED EXHAUST COOLING
    • Publication number 20160169108
    • Publication date Jun 16, 2016
    • United Technologies Corporation
    • Donald W. Peters
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    THREE STREAM, VARIABLE AREA, VECTORABLE NOZZLE
    • Publication number 20150128561
    • 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

    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

    NACELLE FOR AN AIRCRFT BYPASS TURBOJET ENGINE
    • Publication number 20140086738
    • Publication date Mar 27, 2014
    • Aircelle
    • Nicolas DEZEUSTRE
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    ENGINE FOR USE IN AN AERIAL VEHICLE
    • Publication number 20140047816
    • Publication date Feb 20, 2014
    • GROLLO AEROSPACE
    • Mark Grollo
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    TURBINE ENGINE EXHAUST NOZZLE FLAP
    • Publication number 20130327847
    • Publication date Dec 12, 2013
    • United Technologies Corporation
    • Francis R. Moon
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    LINER ASSEMBLY
    • Publication number 20130318978
    • Publication date Dec 5, 2013
    • Christopher Treat
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    Linked Ring Petal Actuation for Variable Area Fan Nozzle
    • Publication number 20130306755
    • Publication date Nov 21, 2013
    • THE BOEING COMPANY
    • Rainer Dittmann
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    VARIABLE AREA FAN NOZZLE AND THRUST REVERSER
    • Publication number 20120325930
    • Publication date Dec 27, 2012
    • Edward B. Pero
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    NOISE REDUCTION OF SUPERSONIC JET ENGINES
    • Publication number 20120255806
    • Publication date Oct 11, 2012
    • Lockheed Martin Corporation
    • Anthony R. Pilon
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    VARIABLE AREA FAN NOZZLE AND THRUST REVERSER
    • Publication number 20120005999
    • Publication date Jan 12, 2012
    • Edward B. Pero
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    NOZZLE-AREA RATIO FLOAT BIAS
    • Publication number 20110088403
    • Publication date Apr 21, 2011
    • United Technologies Corporation
    • Timothy A. Swanson
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    Multifunctional propulsive system for an airplane
    • Publication number 20110030339
    • Publication date Feb 10, 2011
    • AIRBUS OPERATIONS (SAS)
    • Olivier CAZALS
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Application

    VARIABLE AREA FAN NOZZLE AND THRUST REVERSER
    • Publication number 20100257841
    • Publication date Oct 14, 2010
    • Edward B. Pero
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    EXHAUST NOZZLE SEAL WITH SEGMENTED BASESHEET
    • Publication number 20090217671
    • Publication date Sep 3, 2009
    • Darrell Glenn Senile
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS