A directional valve for a fire suppression system comprises a valve member for controlling the discharge of fire suppression agent. The valve member comprises: a blocking portion to provide a closed setting for the fire suppression agent; a first orifice to provide a fully open setting for the fire suppression agent; and a second orifice to provide a restricted opening setting in which discharge of fire suppression agent is restricted. The valve member is configured so that during activation of the directional valve from a closed setting, the first orifice follows the blocking portion and precedes the second orifice in order to provide a fully open setting followed by a restricted opening setting.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    FIRE SUPPRESSION CONTROL SYSTEM FOR AN AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    2017-01-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    A62C FIRE-FIGHTING , Feuerbekämpfung / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT WITH FIRE SUPPRESSION CONTROL SYSTEM

    GATSONIDES JOSEPHINE G / RENNIE PAUL A / SMITH STUART M | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT WITH FIRE SUPPRESSION CONTROL SYSTEM

    GATSONIDES JOSEPHINE G / RENNIE PAUL A / SMITH STUART M | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT FIRE SUPPRESSION SYSTEM

    PARTRIDGE GRANT / GEKELER ANDREAS / MEISLITZER BORIS et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft fire suppression system

    PARTRIDGE GRANT / GEKELER ANDREAS / MEISLITZER BORIS et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT FIRE SUPPRESSION SYSTEM

    PARTRIDGE GRANT / GEKELER ANDREAS / MEISLITZER BORIS et al. | Europäisches Patentamt | 2019

    Freier Zugriff