TREA

Edward B. Thayer

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  • Jupiter, FL, US
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Patents Grantslast 30 patents

  • Information Patent Grant

    Vectoring nozzle using injected high pressure air
    • Patent number 5,706,650
    • Issue date Jan 13, 1998
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Rocket nozzle for a rocket engine
    • Patent number 5,683,033
    • Issue date Nov 4, 1997
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Rocket nozzle for a rocket engine
    • Patent number 5,619,851
    • Issue date Apr 15, 1997
    • United Technologies Corporation
    • Donald E. Johnson
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Hexagonal cluster nozzle for a rocket engine
    • Patent number 5,343,698
    • Issue date Sep 6, 1994
    • United Technologies Corporation
    • Lane Porter
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Gas turbine vectoring exhaust nozzle
    • Patent number 5,335,489
    • Issue date Aug 9, 1994
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Convertible plug nozzle
    • Patent number 5,292,069
    • Issue date Mar 8, 1994
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Axisymmetric nozzle with gimbled unison ring
    • Patent number 5,261,605
    • Issue date Nov 16, 1993
    • United Technologies Corporation
    • George H. McLafferty
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Aircraft reverser port door
    • Patent number 5,209,432
    • Issue date May 11, 1993
    • United Technologies Corporation
    • Gary D. Roberge
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    In-flight reverser
    • Patent number 5,161,752
    • Issue date Nov 10, 1992
    • United Technologies Corporation
    • Jefre H. Cockerham
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    In-flight reverser
    • Patent number 5,150,862
    • Issue date Sep 29, 1992
    • United Technologies Corporation
    • Jefre H. Cockerham
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Gas turbine spherical exhaust nozzle
    • Patent number 4,993,641
    • Issue date Feb 19, 1991
    • United Technologies Corporation
    • Debora F. Kehret
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Yaw thrust vectoring exhaust nozzle
    • Patent number 4,848,664
    • Issue date Jul 18, 1989
    • United Technologies Corporation
    • Edward B. Thayer
    • 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

    Divergent flap actuation system for a two-dimensional exhaust nozzle
    • Patent number 4,819,876
    • Issue date Apr 11, 1989
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Control vent for diverting exhaust nozzle
    • Patent number 4,805,401
    • Issue date Feb 21, 1989
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Area controlled, thrust vectoring vane cascade with nutating contro...
    • Patent number 4,798,328
    • Issue date Jan 17, 1989
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Linkage for area controlled, thrust vectoring vane cascade
    • Patent number 4,760,960
    • Issue date Aug 2, 1988
    • United Technologies Corporation
    • Eric J. Ward
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Two dimensional gas turbine engine exhaust nozzle
    • Patent number 4,753,392
    • Issue date Jun 28, 1988
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    2-D propulsive lift nozzle
    • Patent number 4,714,197
    • Issue date Dec 22, 1987
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Thrust reverser/exhaust nozzle assembly for a gas turbine engine
    • Patent number 4,591,097
    • Issue date May 27, 1986
    • The United States of America as represented by the Secretary of the Air Force
    • Edward B. Thayer
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • 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

    Flap-type two-dimensional nozzle having a plug
    • Patent number 4,005,823
    • Issue date Feb 1, 1977
    • United Technologies Corporation
    • Edward B. Thayer
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Flap-type two-dimensional nozzle
    • Patent number 3,973,731
    • Issue date Aug 10, 1976
    • United Technologies Corporation
    • Edward B. Thayer
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS