Rotor drive and control system for a high speed rotary wing...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 27/00 (2006.01) A47C 21/04 (2006.01)

Patent

CA 2609943

A drive system for a high speed rotary-wing aircraft includes a combiner gearbox in meshing engagement with a main gearbox. The combiner gearbox is driven by one or more engines such that a main rotor system and a translational thrust system are driven thereby. The engine drives the combiner gearbox and thus the main gearbox through an overrunning clutch. The drive system permits the main rotor system RPM to be controlled by offloading power to the translational thrust system during a high speed flight profile.

L'invention concerne un système d'entraînement pour un aéronef à voilure tournante à grande vitesse, comprenant une boîte d'engrenages de transfert en prise par engrènement avec une boîte d'engrenages principale. La boîte d'engrenages de transfert est entraînée par un ou plusieurs moteurs de sorte qu'un système de rotor principal et un système de poussée de translation sont entraînés. Le moteur entraîne la boîte d'engrenages de transfert et ainsi la boîte d'engrenages principale par l'intermédiaire d'un embrayage à roue libre. Le système d'entraînement permet au RPM du système de rotor principal d'être commandé par décharge de puissance vers le système de poussée de translation au cours d'un profil de vol à grande vitesse.

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