Rotor and aircraft passively stable in hover

Details Rotor and aircraft passively stable in hover Rotor and aircraft passively stable in hover

B - Operations, Transporting

64

C

B64C 27/473 (2006.01) B64C 27/10 (2006.01) B64C 27/43 (2006.01) B64C 27/467 (2006.01) B64C 27/52 (2006.01) B64C 27/82 (2006.01)

Patent

CA 2496385

The present invention discloses a rotor that enables an aircraft to be passively stable in hover. The rotor, having a generally fixed geometry is tiltably connected to its rotor shaft. The outer part of the rotor blades have a pitch fixed relative to the rotational plane, whereas the inner part of the rotor blades have a pitch fixed relative to a reference plane perpendicular to the rotor shaft.

L'invention concerne un rotor qui permet à un aéronef d'être passivement stable en vol stationnaire. Le rotor, qui présente une géométrie généralement fixe, est relié à son arbre de rotor de façon à pouvoir pivoter. La partie extérieure des pales du rotor ont un pas fixe par rapport au plan de rotation, alors que la partie intérieure des pales du rotor ont un pas fixe par rapport à un plan de référence perpendiculaire à l'arbre du rotor.

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