Patent ID: 9409650
Filing Date: 2016-08-09
CPC Classification: B64D,F02K,F05D,Y02T

Claim Text:
1. An aircraft nacelle comprising: a thrust reverser device comprising at least one movable cowl; a supporting structure configured to support the thrust reverser device, the supporting structure comprising: at least one base body extending along a longitudinal direction of the nacelle and made from a composite material, wherein open walls of the base body form an open L-shaped bending section such that the entire base body in the form of the open L-shaped bending section provides access to an inner surface of the supporting structure from outside of the supporting structure, and a plurality of reinforcements attached on the inner surface of the supporting structure and distributed along the longitudinal direction, the reinforcements comprising a plurality of cores and plies draping the cores, wherein the cores and the plies are integrated with at least one open wall of the base body and form a portion of the open L-shaped bending section.