A system for managing thermal transfer in an aircraft includes a fuel stabilization unit, a fuel-air heat exchanger, and a turbine. The fuel-air heat exchanger is located downstream from the fuel stabilization unit. The fuel-air heat exchanger places deoxygenized fuel in a heat exchange relationship with compressor bleed air to produce heated deoxygenized fuel and cooled bleed air. The turbine is operationally connected to the engine compressor and receives cooled bleed air from the fuel-air heat exchanger.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Small engine cooled cooling air system


    Beteiligte:

    Erscheinungsdatum :

    2017-02-28


    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



    Small engine cooled cooling air system

    RHODEN WILLIAM E / JALBERT PETER L / BEAUPRE RUDOLPH THOMAS et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    External cooling system of water-cooled engine

    ZHOU ZHENFEI | Europäisches Patentamt | 2021

    Freier Zugriff

    Development of Oil-Cooled Engine for Optimization of Engine Cooling System

    Kitayama, Amane / Tanaka, Koichi / Arase, Kunio | SAE Technical Papers | 2016


    Gas turbine engine in-board cooled cooling air system

    LO CHARLES | Europäisches Patentamt | 2016

    Freier Zugriff

    Gas turbine engine in-board cooled cooling air system

    LO CHARLES | Europäisches Patentamt | 2019

    Freier Zugriff