Abstract: A pivoting door type thrust reverser assembly for a dual flow engine incls a fixed cowling construction with a front body portion (9) and a rear body portion (12) joined by longitudinal beams (10,11) and defining reversal chambers in each of which a door (7) is pivotably received. The door pivot pins (17) are carried by two pairs of struts (15,16) such that the pivot pins are spaced from the engine axis X-X'.
Type:
Grant
Filed:
November 21, 1997
Date of Patent:
August 3, 1999
Assignee:
Societe de Construcion des Avions Hurel-Dubois (societe anonyme