Which component allows rotor blades to flap as a unit in a semi-rigid rotor system?

Study for the FAA Helicopter Flying Test. Utilize flashcards and multiple-choice questions, with each offering hints and explanations. Prepare effectively for your exam!

Multiple Choice

Which component allows rotor blades to flap as a unit in a semi-rigid rotor system?

Explanation:
The ability for rotor blades to flap as a unit in a semi-rigid rotor system comes from the teetering hinge at the rotor hub. This single hinge lets the blades pivot together in a flapping motion, like a seesaw, absorbing lift loads and allowing the rotor disk to tilt slightly under load without the complexity of multiple flapping hinges. The other components play different roles: the Constant Velocity Joint is part of the drive train, not the rotor head; the swashplate translates pilot cyclic and collective inputs to blade pitch changes; and the pitch link connects the pitch horn to the swashplate to modify blade pitch, not the flapping action.

The ability for rotor blades to flap as a unit in a semi-rigid rotor system comes from the teetering hinge at the rotor hub. This single hinge lets the blades pivot together in a flapping motion, like a seesaw, absorbing lift loads and allowing the rotor disk to tilt slightly under load without the complexity of multiple flapping hinges. The other components play different roles: the Constant Velocity Joint is part of the drive train, not the rotor head; the swashplate translates pilot cyclic and collective inputs to blade pitch changes; and the pitch link connects the pitch horn to the swashplate to modify blade pitch, not the flapping action.

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