The invention relates to an aircraft pod equipped with a thrust reverser (62), comprising:-at least one deflection system configured, in an activated state, to direct a flow of air directed in the pod towards a lateral opening (64) of the pod; -at least one orientation system (74) comprising: o at least one transverse deflector (76) configured to direct the air flow deflected by the deflection system (72) in a radial direction and towards the upstream end of the pod; at least one longitudinal deflector (78) intersecting the transverse deflector and oriented in a direction forming an angle of less than 25 DEG with the longitudinal direction. The longitudinal deflector makes it possible to increase the efficiency of the transverse deflector.
本发明涉及一种配备有反推力装置(62)的飞行器吊舱,其包括:‑至少一个偏转系统,其被构造成在启用状态下将吊舱中受到引导的空气流朝吊舱的侧向开口(64)引导;‑至少一个定向系统(74),包括:o至少一个横向偏转器(76),其被构造成沿径向方向并朝吊舱的上游端引导由偏转系统(72)所偏转的空气流;o至少一个纵向偏转器(78),其与横向偏转器相交并且沿与纵向方向形成小于25°的角度的方向定向。纵向偏转器使得允许提高横向偏转器的效率。
Aircraft pod equipped with thrust reverser comprising longitudinal deflector, and aircraft
配备包括纵向偏转器的反推力装置的飞行器吊舱及飞行器
2025-03-21
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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