A surface heat exchanger is provided which utilizes forward and aft brackets to retain the heat exchanger in position. The surface heat exchanger includes a plurality of core cooling channels as well as fins which are disposed for air flow through the gas turbine engine. The brackets include a low-friction wear material as well as an isolator sheet which provides some spring force on the heat exchanger.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Surface cooler support mechanism



    Erscheinungsdatum :

    2017-06-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    SURFACE COOLER SUPPORT MECHANISM

    HUNDLEY WALTER ARTHUR JR / DREISCHARF DEREK THOMAS / DRAKE MARK PHILLIP et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    SURFACE COOLER SUPPORT MECHANISM

    WALTER ARTHUR HUNDLEY JR / DEREK THOMAS DREISCHARF / DATTU G V JONNALAGADDA et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    AIRCRAFT SURFACE COOLER ASSEMBLY

    JIANG HUA / LIGHTHILL ANTHONY LYNN / MOORE JAMES MICHAEL et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Portable cooler with integrated support trays

    WHITNEY CHRISTOPHER WILLIAM / COELHO VITOR | Europäisches Patentamt | 2022

    Freier Zugriff

    Surface cooler having channeled fins

    POLLARD BERWYN OWAIN / SCOTT DAVID RUSSELL | Europäisches Patentamt | 2019

    Freier Zugriff