A nozzle assembly for an ejection seat may comprise a servo valve assembly, a reservoir a cylinder, a nozzle manifold housing comprising a monolithic body having internal manifold structures integral to the body configured to communicate a gas between a pressure source and the reservoir, 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 linear nozzle coupled to the rack piston and configured to rotate in response to an axial translation of the rack piston.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Hydraulic thrust vector pitch control nozzle for rocket catapult


    Beteiligte:

    Erscheinungsdatum :

    2022-05-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    HYDRAULIC THRUST VECTOR PITCH CONTROL NOZZLE FOR ROCKET CATAPULT

    MASTROLIA BRADLEY | Europäisches Patentamt | 2021

    Freier Zugriff

    HYDRAULIC THRUST VECTOR YAW CONTROL FOR ROCKET CATAPULT MOTOR ASSEMBLY

    MASTROLIA BRADLEY | Europäisches Patentamt | 2021

    Freier Zugriff

    Hydraulic thrust vector yaw control for rocket catapult motor assembly

    MASTROLIA BRADLEY | Europäisches Patentamt | 2022

    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 | 2021

    Freier Zugriff