TREA

Pierre M. V. E. Schroer

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  • Brunoy, FR
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Patents Grantslast 30 patents

  • Information Patent Grant

    Aerodynamic fuel injection system for a gas turbine engine
    • Patent number 6,035,645
    • Issue date Mar 14, 2000
    • Societe National d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
    • Mehdi Bensaadi
    • F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
  • Information Patent Grant

    Gas turbine diffuser
    • Patent number 5,592,820
    • Issue date Jan 14, 1997
    • Societe National D'Etdue et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
    • Jean-Paul D. Alary
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    Perforated wall for a gas turbine engine
    • Patent number 5,590,531
    • Issue date Jan 7, 1997
    • Societe National D'Etdue et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
    • Michel A. A. Desaulty
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    System for cooling a high power fuel injector of a dual injector
    • Patent number 5,577,386
    • Issue date Nov 26, 1996
    • Societe Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
    • Jean-Paul D. Alary
    • F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
  • Information Patent Grant

    System for supplying fuel to and cooling a fuel injector of a dual...
    • Patent number 5,568,721
    • Issue date Oct 29, 1996
    • Societe Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
    • Jean-Paul D. Alary
    • F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
  • Information Patent Grant

    Gas-flow separator for a double dome gas turbine engine combustion...
    • Patent number 5,528,896
    • Issue date Jun 25, 1996
    • Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
    • Jean-Paul D. Alary
    • F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
  • Information Patent Grant

    Separator for an annular gas turbine combustion chamber
    • Patent number 5,417,069
    • Issue date May 23, 1995
    • Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
    • Jean-Paul D. Alary
    • F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES