Hybrid-use rotary-wing aircraft with aligned drivetrain
AssigneeRoze Mobility
InventorGrégoire BOURGUIGNON
Life of this patent
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Abstract
Rotary-wing aircraft, comprising: a drive motor (12) with a motor output shaft (12-3), a transfer gearbox (14) having the motor output shaft (12-3) as an input and having a first output (14-1) and a second output (14-2), a cockpit with associated cockpit electronics, a rotary wing with rotor and blades, a tail and tail rotor (20) with a drive shaft (20-1) for driving the tail rotor, and a skids unit with equipment suited to the intended application, characterized in that the motor shaft (12-3) of the motor (12), the transfer gearbox (14) with its second output (14-2) and the drive shaft (20-1) that drives the tail rotor (20) are aligned.
Claims10
A rotary wing aircraft, comprising:
- a drive motor (12) with a motor output shaft (12-3),
- a transfer gearbox (14) having the motor output shaft (12-3) as an input and having a first output (14-1) and a second output (14-2),
- a cockpit (22) with cockpit electronics,
- a rotary wing (16) with rotor (16-1) and blades (16-2),
- a tail (18) and its tail rotor (20) with a drive shaft (20-1) for said tail rotor, and
- a skids unit (24) with equipment suited to the intended application,
- characterized in that the drive shaft (12-3) of the motor (12), the transfer gearbox (14) with its second output (14-2) and the drive shaft (20-1) of the tail rotor (20) are aligned.
Dependencies are inferred from the claim text.