A motor cap assembly for an ejection seat may comprise a servo valve assembly, a reservoir a cylinder, a motor cap manifold housing comprising a monolithic body having an internal manifold structure integral to the body configured to communicate a gas between a pressure source and a gas block, and configured to communicate a hydraulic fluid between, the reservoir, the servo valve assembly, and the cylinder, a rack piston disposed within the cylinder and configured to translate axially therein between a base end and a head end of the cylinder, and a motor cap outer housing coupled circumferentially about the motor cap manifold housing, wherein the motor cap outer housing is configured to rotate circumferentially about the motor cap manifold housing in response to an axial translation of the rack piston.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HYDRAULIC THRUST VECTOR YAW CONTROL FOR ROCKET CATAPULT MOTOR ASSEMBLY


    Beteiligte:

    Erscheinungsdatum :

    2021-09-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Hydraulic thrust vector yaw control for rocket catapult motor assembly

    MASTROLIA BRADLEY | Europäisches Patentamt | 2022

    Freier Zugriff

    Hydraulic thrust vector pitch control nozzle for rocket catapult

    MASTROLIA BRADLEY | Europäisches Patentamt | 2022

    Freier Zugriff

    HYDRAULIC THRUST VECTOR PITCH CONTROL NOZZLE FOR ROCKET CATAPULT

    MASTROLIA BRADLEY | Europäisches Patentamt | 2021

    Freier Zugriff

    VARIABLE THRUST CATAPULT

    WHELAN PATRICK / SALOIS MATTHEW D / BENJAMIN JEFF et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Variable thrust catapult

    BENJAMIN JEFF / SALOIS MATTHEW D | Europäisches Patentamt | 2022

    Freier Zugriff