The invention relates to an aircraft pod (54) equipped with a thrust reverser (62), the device comprising:-at least one deflection system (72) configured to deflect, in an activated state, an air flow (60) conducted in the pod (54) towards a lateral opening (64) of the pod (54); and at least one orientation system (74). The orientation system (74) comprises: o at least one lateral deflector (76) configured to orient the air flow (60) deflected by the deflection system (72) towards the upstream end of the pod (54); o at least one downstream deflector (86) positioned at a downstream edge of the lateral opening (64) and configured to deflect the air flow deflected by the deflection system (72) towards an upstream end of the pod (54). The downstream deflector (86) allows the airflow generated by the thrust reverser (62) to be deflected such that it does not impinge on the downstream edge of the lateral opening (64).
本发明涉及一种配备反推装置(62)的飞行器吊舱(54),该装置包括:‑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(60)朝吊舱(54)的侧向开口(64)偏转;‑至少一个定向系统(74)。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(60)朝吊舱(54)的上游端定向;o至少一个下游偏转器(86),其定位于侧向开口(64)的下游边缘处,并被构造为能够将偏转系统(72)所偏转的空气流朝吊舱(54)的上游端偏转。下游偏转器(86)允许偏转由反推装置(62)产生的空气流,从而使得其不会冲击侧向开口(64)的下游边缘。
Aircraft pod and aircraft comprising propulsion assembly having such aircraft pod
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
2024-10-29
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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