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公开(公告)号：US20230192279A1
公开(公告)日：2023-06-22
申请号：US17989077
申请日：2022-11-17
发明人： Jerome GENEIX , Mikolaj LUSZCZYNSKI
CPC分类号： B64C27/24 , B64D27/24 , B64D35/00 , B60L53/00 , G05D1/102 , H02K7/14 , H01M10/46 , B60L2200/10 , H01M2220/20
摘要： A rotary wing aircraft that extends along a roll axis between a nose region and an aft region, comprising: at least one first single-blade rotor and at least one second single-blade rotor which are spaced apart from each other along the roll axis; at least one first electric machine and at least one second electric machine which are at least configured to drive in motor mode the at least one first single-blade rotor and the at least one second single-blade rotor for generating lift in hover condition of the rotary wing aircraft; at least one propulsion device that is at least configured to generate forward thrust in forward flight condition of the rotary wing aircraft; and a fixed-wing arrangement that is at least configured to provide lift in the forward flight condition.
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2.发明申请公开(公告)号：US20210163125A1
公开(公告)日：2021-06-03
申请号：US17099064
申请日：2020-11-16
申请人： AIRBUS HELICOPTERS
发明人： Oliver BARAIS , Paul EGLIN , Jerome GENEIX
IPC分类号： B64C27/06 , B64C27/82 , B64D27/02 , B64D27/24 , B64D35/04 , B64D31/00 , B64C5/02 , B64C3/32 , B64C11/46 , B64D27/04 , B64D27/10 , B64D31/04
摘要： A rotorcraft including a first power plant, at least one main rotor participating at least in providing lift for the rotorcraft in the air, and at least one tail rotor carried by a tail boom, the first power plant including at least one engine. In accordance with the invention, the rotorcraft includes: at least one pusher or puller propeller independent from the at least one main rotor, the at least one pusher or puller propeller participating at least in providing propulsion or traction for the rotorcraft; a second power plant including at least one electric motor; and at least one control member configured to generate a control setpoint or instruction for controlling the at least one electric motor.
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公开(公告)号：US20230323941A1
公开(公告)日：2023-10-12
申请号：US18121861
申请日：2023-03-15
申请人： AIRBUS HELICOPTERS
发明人： Stephane DEPORT , Olivier BARAIS , Jerome GENEIX
CPC分类号： F16H57/0441 , F16H57/0438 , F16H57/0443 , F16H57/0442 , F16N7/02 , F16N7/385 , F16N2210/12 , F16N2250/04 , F16N2260/04 , F16N2260/06 , F16N2260/08 , F16H2057/02043
摘要： A mechanical system comprising a sump and at least one component to be lubricated or cooled arranged in the sump, the mechanical system comprising a lubricating fluid system provided with a lubricating fluid and a tank arranged in the sump. The tank is a leaking tank and is situated above said at least one component to be lubricated or cooled, the lubricating fluid flowing out of the tank by force of gravity, so as to reach said at least one component to be lubricated or cooled. The lubricating fluid system has at least one lift flow generator connected by at least one filling line to the tank and to at least one suction point present in a bottom of the sump. The lift flow generator fills the tank with the lubricating fluid present in said bottom at least during a starting phase.
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