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Subspace thrust type cascade for a motor turbojato of aircraft and aircraft engine nacelle oara a turbojato
Subspace thrust type cascade for a motor turbojato of aircraft and aircraft engine nacelle oara a turbojato
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机译:飞机和飞机发动机短舱涡轮喷气发动机的子空间推力型叶栅
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摘要
A cascade-type thrust reverser for an aircraft turbojet engine includes a front frame, a sliding cowl between a direct jet position and a reverse jet position, a plurality of actuating cylinders interposed between this front frame and this sliding cowl, and a plurality of cascades pivotally mounted on the front frame between the direct and reverse jet positions. In the direct jet position, the cascades are substantially parallel to the axis (A) of the thrust reverser, and in the reverse jet position, the cascades are inclined relative to the axis (A) of the thrust reverser. In particular, the cascade-type thrust reverser includes a single radial layer of cascades.
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