An annular torsional rigid static component for an aircraft...

F - Mech Eng,Light,Heat,Weapons – 01 – D

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F01D 9/04 (2006.01) B64D 27/10 (2006.01) F01D 25/28 (2006.01)

Patent

CA 2588468

The invention relates to an annular torsional rigid static component for an aircraft engine, the component comprises at least one means (101) for mounting the engine to an aircraft. Said mounting means (101) comprises a body (103) formed in a composite material.

La présente invention concerne un composant statique rigide en torsion annulaire pour un moteur d~avion, le composant comprenant au moins un moyen (101) de fixation du moteur à un avion. Ledit moyen de fixation (101) comprend un corps (103) moulé à partir d~un matériau composite.

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