Autonomic rotor system for an aircraft

Details Autonomic rotor system for an aircraft Autonomic rotor system for an aircraft

B - Operations, Transporting

64

C

B64C 27/52 (2006.01) B64C 27/18 (2006.01)

Patent

CA 2737054

A rotor system for an aircraft including a rotor (1) with a drive part (2) mounted rotatable about a rotation axis (8) and supporting the proximal end (9) of at least one rotor blade (3).The rotor system comprises a jet turbine (4) for providing pressurised exhaust gas to a rotary structure(7) having at least one jet nozzle outlet (6) and at least one jet stream duct (5) for transporting the pressurised exhaust gas from the turbine (4) to the jet nozzle outlet (6) to cause rotation of the rotary structure (7) by expelling the pressurised exhaust gas through the nozzle outlet (6). In addition, only the rotary structure(7) and not the rotor blade (3) comprise a jet stream duct (5) and a nozzle outlet (6).

L'invention concerne un système de rotor destiné à un avion. Ce système comprend un rotor (1) doté d'une partie d'entraînement (2) montée rotative autour d'un axe de rotation (8) et servant de support à l'extrémité proximale (9) d'au moins une pale de rotor (3). Le système de rotor comprend une turbine à réaction (4) servant à produire des gaz d'échappement sous pression pour une structure rotative (7) présentant au moins une sortie de tuyère (6) et au moins un conduit de courants-jet (5) conçu pour transporter les gaz d'échappement sous pression de la turbine (4) à la sortie de tuyère (6) afin de mettre la structure rotative (7) en rotation par expulsion des gaz d'échappement sous pression par la sortie de tuyère (6). En outre, seule la structure rotative (7), et non la pale (3), comprend un conduit de courants-jet (5) et une sortie de tuyère (6).

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