Patent ID: 8840061

Claim:
A strut adapted to support an aircraft turbojet engine nacelle, the strut comprising: a connecting part for connecting a casing of a fan or a casing of a gas generator of said turbojet engine and a wing of said aircraft, and a Y-shaped box-section part, secured to said connecting part and forming an upper part of an internal fixed structure of said nacelle, the Y-shaped box-section having a lower central wall connected to two upper lateral walls to define a hollow part without any internal stiffening members, the two upper lateral walls further defining platens to secure the Y-shaped box-section part to an upstream part of the gas generator, wherein the connecting part of the strut is fixed on said casing of the fan or on said casing of the gas generator, and thrust recovery connecting rods extending inside of the hollow part of the Y-shaped box-section part of said strut to cooperate with said casing of the gas generator.