Rotor blade flap driving apparatus
AssigneeAdvanced Technology Institute of Commuter-Helicopter, Ltd.
InventorsEiichi Yamakawa, Tatsuro Hongu
Life of this patent
Estimating the term…
Loading patent…
AssigneeAdvanced Technology Institute of Commuter-Helicopter, Ltd.
InventorsEiichi Yamakawa, Tatsuro Hongu
Estimating the term…
An actuator and first to fourth links constitute a first displacement magnifying mechanism. An input shaft which is fixed in a basal end of the first and second links, a support shaft which is fixed in a basal end of the third and fourth links, and a displacement magnifying lever constitute a second displacement magnifying mechanism. In the displacement magnifying lever, an intermediate portion is angularly displaceably coupled to a tip end of the support shaft, a tip end of the input shaft is angularly displaceably coupled to one end, and an output rod is angularly displaceably coupled to another end. The expansion and contraction of the actuator are magnified by the first and second displacement magnifying mechanisms so as to drive a flap angularly via output rod. According to this configuration, the displacement of the actuator can be largely magnified so that the flap can be sufficiently angularly displaced in the vertical direction and in a reciprocal manner.
A rotor blade flap driving apparatus comprising:
Dependencies are inferred from the claim text.