The invention relates to an aircraft pod (54) equipped with a thrust reverser (62) comprising:-at least one longitudinal actuator (86) to activate or deactivate the thrust reverser; -at least one deflection system (72) configured to deflect, in an activated state, an air flow conducted in the pod (54) towards a lateral opening (64) of the pod (54); -at least one orientation system (74) comprising: o at least one lateral deflector (76) configured to be able to orient the air flow deflected by the deflection system (72) towards the upstream end of the pod (54); o, for each longitudinal actuator (86), a hollow longitudinal deflector (90) configured to receive the longitudinal actuator (86) and comprising an aerodynamic profile having a leading edge edge oriented towards the deflection system (72).

    本发明涉及一种配备有反推装置(62)的飞行器吊舱(54),反推装置包括:‑至少一个纵向致动器(86)以激活或停用反推装置;‑至少一个偏转系统(72),其被构造为能够在激活状态下将在吊舱(54)中引导的空气流朝吊舱(54)的侧向开口(64)偏转;‑至少一个定向系统(74),包括:o至少一个横向偏转器(76),其被构造为能够将偏转系统(72)所偏转的空气流朝吊舱(54)的上游端定向;o针对每个纵向致动器(86)的中空的纵向偏转器(90),其被构造为能够容纳纵向致动器(86),并包括具有朝偏转系统(72)定向的前缘边缘的空气动力学轮廓。


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    Title :

    Aircraft pod and aircraft comprising same


    Additional title:

    飞行器吊舱及包括其的飞行器


    Contributors:

    Publication date :

    2024-12-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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