A turbojet engine with two thrust reverser modules. Each module includes an outer casing, an inner casing and a securing system for securing the inner casing to the outer casing which comprises first and second hoods. A housing between the hoods has a securing wall, a seal with a sausage secured to the securing wall, and a crusher rigidly secured to the second hood and arranged so as to crush the sausage towards the securing wall when the second hood goes from the spaced-apart position to the close-together position. Therefore, the sausage moves in the longitudinal direction, thus limiting shearing of the seal and transverse movements owing to the manufacturing and assembly tolerances and the movements in flight.
TURBORÉACTEUR D'AÉRONEF COMPORTANT DEUX MODULES D'INVERSION DE POUSSÉE
TURBOJET ENGINE OF AN AIRCRAFT COMPRISING TWO THRUST REVERSER MODULES
TRIEBWERK EINES LUFTFAHRZEUGS MIT ZWEI SCHUBUMKEHRMODULEN
2023-12-20
Patent
Electronic Resource
French
turboreacteur double flux comportant un système d’inversion de poussée
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