The invention relates to an aircraft pod equipped with a thrust reverser (62), the device comprising:-at least one deflection system configured to deflect, in an activated state, an air flow directed in the pod towards a lateral opening (64) of the pod; and at least one orientation system (74). The orientation system (74) comprises: o at least one transverse deflector (76) configured to orient the air flow deflected by the deflection system (72) in a radial direction and towards the upstream end of the pod; and at least one longitudinal deflector (78) configured to orient the air flow deflected by the deflection system in at least one direction forming an angle with the radial direction. The longitudinal deflector allows the airflow generated by the thrust reverser to be deflected such that the operation of the probe positioned on the outer surface of the pod is not disturbed.

    本发明涉及一种配备有反推装置(62)的飞行器吊舱,该装置包括:‑至少一个偏转系统,其被构造为能够在激活状态下将在吊舱中引导的空气流朝吊舱的侧向开口(64)进行偏转;‑至少一个定向系统(74)。该定向系统(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)所偏转的空气流沿径向方向并朝吊舱的上游端进行定向;o至少一个纵向偏转器(78),其被构造为能够将偏转系统所偏转的空气流沿与径向方向形成角度的至少一个方向进行定向。纵向偏转器允许偏转反推装置产生的空气流,从而使得不干扰定位于吊舱的外表面上的探头的运行。


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    Title :

    Aircraft pod and aircraft comprising propulsion assembly having such aircraft pod


    Additional title:

    飞行器吊舱及包括具有该飞行器吊舱的推进组件的飞行器


    Contributors:

    Publication date :

    2024-10-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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