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REDUCED POWER INDIVIDUAL BLADE CONTROL SYSTEM ON A ROTORCRAFT
REDUCED POWER INDIVIDUAL BLADE CONTROL SYSTEM ON A ROTORCRAFT
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机译:降低了桨叶机的功率单叶片控制系统
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摘要
An aircraft comprising an airframe; a rotor system mounted to the airframe, the rotor system including a plurality of rotor blades, each of the plurality of rotor blades including a root portion extending to a tip portion through an airfoil portion, the airfoil portion having a leading edge and a trailing edge; at least one control surface mounted within the airfoil portion of at least one of the plurality of rotor blades; at least one actuator configured to actuate the at least one control surface; and at least one actuator configured to pitch at least one of the plurality of rotor blades about a blade pitch axis
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