Apparatuses and systems that use a variable displacement motor-pump (VDMP) to control the position and speed of a hose for an aerial refueling system are disclosed. At displacements greater than required to hold a position of the hose, the VDMP operates in a motor mode to retract the hose. For lesser displacements, the VDMP operates in a pump mode to control extension of the hose. In accordance with some embodiments, a pump-motor relief valve operates to throttle hydraulic fluid flow from the VDMP and to control mixing of hydraulic fluid flowing from the VDMP with system hydraulic fluid.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Hydraulic motor assembly for an aerial refueling system


    Beteiligte:
    BARTOV ASHER (Autor:in) / KUBILOS CHARLES (Autor:in)

    Erscheinungsdatum :

    11.08.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein / F16H Getriebe , GEARING



    Hydraulic motor assembly for an aerial refueling system

    BARTOV ASHER / KUBILOS CHARLES | Europäisches Patentamt | 2021

    Freier Zugriff

    Aerial refueling system with hydraulic motor assembly comprising multi-orifice bypass

    BARTOV ASHER | Europäisches Patentamt | 2019

    Freier Zugriff

    WING AERIAL REFUELING SYSTEM

    FERGUSON STANLEY D / FIALHO IAN J / POTTER RICHARD C | Europäisches Patentamt | 2015

    Freier Zugriff

    Wing aerial refueling system

    FERGUSON STANLEY D / FIALHO IAN J / POTTER RICHARD C | Europäisches Patentamt | 2017

    Freier Zugriff

    WING AERIAL REFUELING SYSTEM

    FERGUSON STANLEY D / FIALHO IAN J / POTTER RICHARD C | Europäisches Patentamt | 2016

    Freier Zugriff