The invention relates to an aircraft propulsion assembly equipped with a thrust reverser device (60), comprising:-at least one side opening (64) through a nacelle (48) of the propulsion assembly configured to be able to be in an open state or a closed state; -at least one inflatable barrier (66) configured to be in a deflated state, in which the barrier (66) does not protrude into the annular duct (50) conducting the air flow (52), and an inflated state, in which the barrier (66) does not protrude into the annular duct (50) conducting the air flow (52); a substantially rigid or semi-rigid barrier (66) deploys and extends through the annular duct (50) to deflect at least a portion of the air flow (52) in a direction towards the side opening (64); -at least one supply system (98) configured to be able to supply a fluid to the inflatable barrier (66). The invention also relates to an aircraft comprising at least one such propulsion assembly.
本发明涉及一种配备有推力反向器装置(60)的飞行器推进组件,其包括:‑至少一个侧开口(64),其穿过推进组件的发动机舱(48),其被构造为能够处于打开状态或关闭状态;‑至少一个可充气的屏障(66),其被构造成处于已泄气状态和充气状态,在已泄气状态下,屏障(66)不突出至引导空气流(52)的环形管道(50)中,而在充气状态下,基本刚性或半刚性的屏障(66)展开并延伸穿过环形管道(50)以使空气流(52)的至少一部分沿朝向侧开口(64)的方向偏转;‑至少一个供应系统(98),其被构造为能够对可充气的屏障(66)供应流体。本发明还涉及一种包括至少一个这种推进组件的飞行器。
Aircraft propulsion assembly equipped with thrust reverser comprising at least one inflatable barrier and aircraft comprising same
配备有包括至少一个可充气屏障的反推装置的飞行器推进组件及包括其的飞行器
16.04.2024
Patent
Elektronische Ressource
Chinesisch
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