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US 2024/0300663 A1Published application
Thrust generator for rotorcraft
AssigneeHonda Motor Co., Ltd.
InventorRyuzaburo KOBAYASHI
Life of this patent
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Abstract
A thrust generator for a rotorcraft includes: a support part detachably mounted to a base provided in the rotorcraft; a rotor shaft rotatably supported by the support part; multiple rotating blades joined to the rotor shaft; and a drive unit detachably mounted to the support part or the base, wherein an output shaft of the drive unit is detachably connected to the rotor shaft.
Claims9
A thrust generator for a rotorcraft, the thrust generator comprising:
- a support part detachably mounted to a base provided in the rotorcraft;
- a rotor shaft rotatably supported by the support part;
- multiple rotating blades joined to the rotor shaft;
- and
- a drive unit detachably mounted to the support part or the base,
- wherein an output shaft of the drive unit is detachably connected to the rotor shaft.
3 more elements
Dependencies are inferred from the claim text.