The invention relates to a thrust group (300) for a propulsion device (10), comprising a thrust engine (302), arranged to provide a thrust force (F1, F2) oriented in a direction so as to provide substantially vertical take-off and landing capability, a deflector assembly (304) comprising a pair of deflecting elements (306a, 306b) arranged to selectively divert the ejected fluid and movably mounted in the fluid outlet path. In order to reduce the bulk of the thrust group and improve reliability and responsiveness, the invention relates more particularly to the positioning of the deflecting elements opposite the ejected fluid.

    本发明涉及一种用于推进装置(10)的推进单元(300),其包括:推进发动机(302),该推进发动机布置成提供推力(F1,F2),该推力沿着方向取向,以便提供基本上竖直的起飞和着陆能力;偏转器组件(304),该偏转器组件包括一对可移动的偏转器元件(306a,306b),其布置成选择性地偏转所喷射的流体并且可移动地安装在流体出口轨迹中。为了减小推进单元的体积并改善其可靠性和响应性,本发明更具体地涉及偏转器元件相对于所喷射的流体的定位。


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    Titel :

    THRUST GROUP FOR A PROPULSION DEVICE AND ASSOCIATED PROPULSION DEVICE


    Weitere Titelangaben:

    用于推进装置的推进单元和相关联的推进装置


    Beteiligte:
    ZAPATA FRANKIE (Autor:in)

    Erscheinungsdatum :

    2022-01-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge



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