Patent Number: 8,793,973

Title: 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.

Inventors: Vauchel; Guy Bernard (Harfleur, FR)

Assignee: Aircelle

International Classification: F02K 3/02 (20060101); B05B 12/00 (20060101); B63H 11/10 (20060101); B63H 25/46 (20060101); F02K 1/00 (20060101)

Expiration Date: 8/05/12018