TREA

Raymond J. Bruchez

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  • Lake Park, FL, US
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Patents Grantslast 30 patents

  • Information Patent Grant

    Attachment means for flaps of variable exhaust nozzle
    • Patent number 5,893,518
    • Issue date Apr 13, 1999
    • United Technologies Corporation
    • Raymond J. Bruchez
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Gas turbine exhaust nozzle flap and flap seal apparatus
    • Patent number 5,839,663
    • Issue date Nov 24, 1998
    • United Technologies Corporation
    • D. Andrew Broadway
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Serviceable liner for gas turbine engine
    • Patent number 5,704,208
    • Issue date Jan 6, 1998
    • Keith S. Brewer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Serviceable liner for gas turbine engine
    • Patent number 5,697,213
    • Issue date Dec 16, 1997
    • Keith S. Brewer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    One-piece flameholder
    • Patent number 5,367,873
    • Issue date Nov 29, 1994
    • United Technologies Corporation
    • W. Kevin Barcza
    • F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
  • Information Patent Grant

    Damper for augmentor liners
    • Patent number 5,201,887
    • Issue date Apr 13, 1993
    • United Technologies Corporation
    • Raymond J. Bruchez
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Thrust vectoring exhaust nozzle
    • Patent number 5,082,182
    • Issue date Jan 21, 1992
    • United Technologies Corporation
    • Raymond J. Bruchez
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Variable convergent/divergent nozzle
    • Patent number 4,799,623
    • Issue date Jan 24, 1989
    • United Technologies Corporation
    • Raymond J. Bruchez
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Partial swirl augmentor for a turbofan engine
    • Patent number 4,203,285
    • Issue date May 20, 1980
    • The United States of America as represented by the Secretary of the Air Force
    • Kurt J. Hanloser
    • F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES