Independent hydraulic control system for rotorcraft secondary rotor
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United States of America Patent
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Nov 14, 2017
Issued Date -
N/A
app pub date -
Jul 1, 2013
filing date -
Jul 1, 2013
priority date (Note) -
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Abstract
According to some embodiments, a rotorcraft includes a secondary rotor control system located proximate to the empennage of the rotorcraft. The secondary rotor control system includes at least one hydraulic pump and at least one hydraulic actuator. The at least one hydraulic pump is located proximate to the empennage. The at least one hydraulic actuator is located proximate to the empennage and configured to adjust at least one operating characteristic of the at least one secondary rotor blade.
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