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US 12,060,149 B2Granted
Pitch angle blocking device
AssigneeAirbus Helicopters Deutschland GmbH
InventorsMoritz Buesing, Bernward Kahl, Markus Bauer
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AssigneeAirbus Helicopters Deutschland GmbH
InventorsMoritz Buesing, Bernward Kahl, Markus Bauer
Estimating the term…
A pitch angle blocking device for blocking the pitch angle of a multi-blade rotor that has neighboring first and second rotor blades in circumferential direction that extend from a rotor hub of a rotary-wing aircraft In non-operational mode of the rotary-wing aircraft. The present embodiments further relate to a multi-blade rotor of a rotary-wing aircraft that is adapted to receiving such a pitch angle blocking device, and to a rotary-wing aircraft with such a multi-blade rotor. The pitch angle blocking device comprises first and second attachment means that are configured to be non-rotatably and releasably attached to the first and second rotor blades spaced apart from the rotor hub, and a connecting device that non-rotatably connects the first attachment means with the second attachment means.
A pitch angle blocking device for blocking a pitch angle of a multi-blade rotor of a rotary-wing aircraft in non-operational mode of the rotary-wing aircraft, the multi-blade rotor having neighboring first and second rotor blades in circumferential direction that extend from a rotor hub that is rotatable around a rotor axis in a rotor plane, comprising:
A pitch angle blocking device for blocking a pitch angle of a multi-blade rotor of a rotary-wing aircraft in non-operational mode of the rotary-wing aircraft, the multi-blade rotor having neighboring first and second rotor blades in circumferential direction that extend from a rotor hub that is rotatable around a rotor axis in a rotor plane, comprising:
Dependencies are inferred from the claim text.