The thrust vectoring apparatus has a nozzle, a jet tab arranged behind the nozzle, a rotation shaft 30 connected to the jet tab, and a gas seal member arranged on an outer circumferential surface of the rotation shaft. The rotation shaft is connected to the jet tab, and has the protrusion in the redial direction out of the rotation shaft on the rear side of the gas seal member. The protrusion restrains that the combustion gas exhausted from the nozzle flows toward the gas seal member.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    THRUST VECTORING APPARATUS AND FLYING OBJECT HAVING THRUST VECTORING APPARATUS


    Beteiligte:
    FUJISAWA FUMINORI (Autor:in) / TANI HIROYUKI (Autor:in) / HYUGA DAISUKE (Autor:in)

    Erscheinungsdatum :

    2016-03-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen



    Thrust vectoring apparatus and flying object having thrust vectoring apparatus

    FUJISAWA FUMINORI / TANI HIROYUKI / HYUGA DAISUKE | Europäisches Patentamt | 2017

    Freier Zugriff

    Thrust vectoring system

    THOMAS CLAYSON / MARK STOKES | Europäisches Patentamt | 2023

    Freier Zugriff

    Thrust vectoring systems

    KING, H. / SCHNELKER, D. | AIAA | 1970


    Thrust vectoring systems

    King, H. J. / Schnelker, D. / Ward, J. W. et al. | NTRS | 1972


    Control of Ducted Fan Flying Object Using Thrust Vectoring

    Miwa, Masafumi / Shigematsu, Yuki / Yamashita, Takashi | Springer Verlag | 2013