The invention relates to a turbine engine module having a longitudinal axis X, comprising: an unducted propeller (2) intended to be driven in rotation about the longitudinal axis X by a power shaft (10, 11) connected to at least one rotor member (5, 6); at least one airflow straightener (3) comprising a plurality of stator vanes (28), the plurality of stator vanes extending along a radial axis Z; at least one first housing (17) mounted upstream of the rotor member (5, 6) along the longitudinal axis and a second housing (33) mounted downstream of the rotor member along the longitudinal axis. According to the invention, the stator vanes (28) each comprise a root (30) housed in a sleeve (37) connected to the first housing (17) and to the second housing (33).

    本发明涉及一种具有纵向轴线X的涡轮发动机模块,该涡轮发动机模块包括:无涵道螺旋桨(2),该无涵道螺旋桨旨在由动力轴(10,11)驱动围绕纵向轴线X旋转,该动力轴连接到至少一个转子构件(5,6);至少一个气流矫直器(3),至少一个气流矫直器包括多个定子轮叶(28),多个定子轮叶沿径向轴线Z延伸;至少一个第一壳体(17)和第二壳体(33),至少一个第一壳体沿纵向轴线安装在转子构件(5,6)的上游,该第二壳体沿纵向轴线安装在转子构件的下游。根据本发明,定子轮叶(28)各自包括容纳在套筒(37)中的根部(30),该套筒连接到第一壳体(17),并且连接到第二壳体(33)。


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    Title :

    Turbine engine module equipped with propeller and stator vanes carried by two housings, and corresponding turbine engine


    Additional title:

    配备有螺旋桨和由两个壳体承载的定子轮叶的涡轮发动机模块以及对应的涡轮发动机



    Publication date :

    2023-06-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




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