Invention Grant
US08793973B2 Thrust reverser for a dual-flow turbine engine nacelle 有权
双流涡轮发动机舱的推力反向器

Thrust reverser for a dual-flow turbine engine nacelle
Abstract:
The invention relates to a thrust reverser (1) for the nacelle of a dual-flow turbine engine, in which the bypass means (4) and the actuation jacks (22) of the sliding cowling (2) and of the reverse flaps (20) are arranged in two substantially parallel planes arranged above one another in the radial direction of the nacelle. The invention also relates to a nacelle for a dual-flow turbine engine that comprises such a thrust reverser.
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