Patent Number: 8,876,018

Title: Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle

Abstract: An arrangement is provided that includes a thrust reverser flap link rod on an internal fixed structure of a turbojet engine nacelle. The link rod is connected to the internal fixed structure by an elastic means that is a spring.

Inventors: Vauchel; Guy Bernard (Harfleur, FR), Segat; Peter (Le Havre, FR)

Assignee: Aircelle

International Classification: B63H 11/00 (20060101); B64D 33/04 (20060101); F02K 1/00 (20060101); F02K 3/02 (20060101); F02K 1/62 (20060101)

Expiration Date: 2019-11-04 0:00:00