A rocket motor assembly (3) for use with an aircraft ejection seat comprises a rocket motor (4) having a rocket motor housing (5) and an exhaust outlet (6-9) to permit exhaust gas to be output from the rocket motor (4) along a thrust vector. The rocket motor assembly (3) comprises a first rotational coupling (12) which is configured to rotationally couple a first part (13) of the rocket motor housing (5) to a support structure (10) and a releasable coupling (14) which is configured to releasably couple a second part (15) of the rocket motor housing (5) to the support structure (10). The releasable coupling (14) is configured to release the second part (15) of the rocket motor housing (5) to permit the rocket motor housing (5) to rotate about the rotational coupling (12) to change the angle of the thrust vector of exhaust gas output from the exhaust outlet (6-9).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rocket Motor Assembly


    Beteiligte:
    RUFF STEPHEN (Autor:in)

    Erscheinungsdatum :

    09.08.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Rocket motor assembly

    RUFF STEPHEN | Europäisches Patentamt | 2019

    Freier Zugriff

    A rocket motor assembly

    Europäisches Patentamt | 2016

    Freier Zugriff

    A rocket motor assembly

    STEPHEN RUFF | Europäisches Patentamt | 2021

    Freier Zugriff

    ROCKET MOTOR

    NANAMEGI KAZUHISA / SATO SOJI / TAKUMA HIROKAZU | Europäisches Patentamt | 2020

    Freier Zugriff

    ROCKET MOTOR

    CESARONI ANTHONY JOSEPH / LARSON JERRY | Europäisches Patentamt | 2024

    Freier Zugriff