An engine cooling system for a rotorcraft includes an engine having an engine cooling circuit, a hydraulic pump powered by the engine to pump hydraulic fluid, and a hydraulic circuit in fluid communication with the hydraulic pump and the engine cooling circuit, the hydraulic circuit including at least one hydraulic-powered component. The hydraulic pump is adapted to pump the hydraulic fluid through both the hydraulic circuit and the engine cooling circuit, thereby cooling the engine.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Engine cooling systems for aircraft


    Beteiligte:

    Erscheinungsdatum :

    2021-06-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F01P Kühlung von Kraft- und Arbeitsmaschinen oder Kraftmaschinen allgemein , COOLING OF MACHINES OR ENGINES IN GENERAL / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein



    ENGINE COOLING SYSTEMS FOR AIRCRAFT

    BRODEUR NICHOLAS | Europäisches Patentamt | 2019

    Freier Zugriff

    ENGINE COOLING SYSTEMS FOR AIRCRAFT

    BRODEUR NICHOLAS | Europäisches Patentamt | 2019

    Freier Zugriff

    Engine Cooling Systems for Aircraft

    BRODEUR NICHOLAS | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft Radial Engine CFD Cooling Model

    Pietrykowski, Konrad / Tulwin, Tytus | SAE Technical Papers | 2014


    OIL COOLING SYSTEM FOR AIRCRAFT ENGINE

    WALZ ANDREW / DOMINGO RITCHIE | Europäisches Patentamt | 2022

    Freier Zugriff