Hub for rotor head of rotary wing aircraft and rotor head...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 27/32 (2006.01) B64C 27/35 (2006.01)

Patent

CA 2251029

The invention concerns a hub and a rotor head for a rotary wing aircraft, comprising a top plate (1) and a bottom plate (4) forming two separate pieces mutually assembled by the insertion of external frames (14) of said spherical stops (8), such that said plates (3, 4) are distant from each other delimiting between them a space in which are housed said spherical stops (8), said external frames (14) being arranged at the periphery of said plates and run through by fixing means (5) mutually integrating said plates (3, 4) and said spherical stops (8).

La présente invention concerne un moyeu et une tête de rotor pour un aéronef à voilure tournante. Selon l'invention, ledit moyeu comprend un plateau supérieur (3) et un plateau inférieur (4) formant deux pièces distinctes assemblées l'une à l'autre avec interposition des armatures externes (14) desdites butées sphériques (8), de sorte que lesdits plateaux (3, 4) sont espacés l'un de l'autre et délimitent entre eux un espace dans lequel sont logées lesdites butées sphériques (8), lesdites armatures externes (14) étant disposées à la périphérie desdits plateaux (3, 4) et étant traversées par des moyens de fixation (5) solidarisant entre eux lesdits plateaux (3, 4) et lesdites butées sphériques (8).

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