A valve and a heat exchanger apparatus for a gas turbine engine include a valve body having a valve seat and an actuation component including a plate formed from a set of metal layers and responsive to a change in at least one of a thermal condition and a pressure exerted thereon such that the plate moves and the valve moves between an opened and a closed position where a portion of the plate engages with the valve seat.


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    Title :

    AVIATION VALVE AND GAS TURBINE ENGINE WITH SAME


    Additional title:

    VANNE D'AVIATION ET TURBINE A GAZ COMPORTANT UNE TELLE VANNE


    Contributors:

    Publication date :

    2018-01-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16K VALVES , Ventile



    General Aviation Turbine Engine (GATE) study

    Baerst, C. F. / Furst, D. G. | NTRS | 1979


    General Aviation Turbine Engine (GATE) Study

    C. F. Baerst / D. G. Furst | NTIS | 1979


    General aviation turbine engine /GATE/ concepts

    Lays, E. J. / Murray, D. L. | NTRS | 1979


    General aviation turbine engine /GATE/ concepts

    LAYS, E. / MURRAY, D. | AIAA | 1979