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    • 64. 发明申请
    • MAGNETIC MOTOR
    • 磁电机
    • WO2013045676A3
    • 2014-02-20
    • PCT/EP2012069283
    • 2012-09-28
    • LODESTONECO ENERGY HOLDING LTD
    • RODRIGUEZ JIMINEZ FRANCISCO
    • H02K51/00H02K49/10H02K53/00
    • H02K51/00H02K49/108H02K53/00
    • A magnetic motor (10) comprising a shaft (14), a drive disc (20) with two peripheral first permanent magnets (22), a propulsion disc (30) with two peripheral second permanent magnets (32) being independently rotatable on the shaft (14). First, the drive disc (20) is speeded up, the propulsion mechanism (40) propels the propulsion disc (30), which impels thereby the drive disc (20) to rotate through interaction of the magnetic fields of first and second magnets (22,32). Than, a braking mechanism (50) brakes the propulsion disc (30), whereby inertia causes the drive disc (20) continous rotation. Than, the propulsion mechanism (40) is prepared to accelerate the momentary stationary propulsion disc (30) and a control mechanism causes the brake (50) to release, if the magnets (22,32) are facing each other. Than, the rotating propulsion disc (30) pushes the drive disc (20) by repulsion of first and second magnets (22, 32).
    • 一种包括轴(14)的磁力马达(10),具有两个周边第一永久磁铁(22)的驱动盘(20),具有两个外围第二永久磁铁(32)的推进盘(30)可在轴 (14)。 首先,驱动盘(20)被加速,推进机构(40)推动推进盘(30),从而推动驱动盘(20)通过第一和第二磁体(22)的磁场的相互作用而旋转 ,32)。 制动机构(50)制动推进盘(30),由此惯性导致驱动盘(20)连续旋转。 如果磁体(22,32)彼此面对,推进机构(40)准备加速瞬时固定推进盘(30)并且控制机构使制动器(50)释放。 旋转的推进盘(30)通过排斥第一和第二磁体(22,32)推动驱动盘(20)。
    • 69. 发明申请
    • ELECTROMAGNETIC POWER TRANSMISSION FOR A ROTARY-WING AIRCRAFT OR A FIXED-WING AIRCRAFT
    • 用于旋转式飞机或固定式飞机的电磁传动
    • WO2013029085A1
    • 2013-03-07
    • PCT/AU2012/000968
    • 2012-08-17
    • CHANTRIAUX, EricCHRETIEN, Pascal
    • CHANTRIAUX, EricCHRETIEN, Pascal
    • H02K16/00H02K51/00H02P9/00
    • F04D13/06B64C27/14B64C2201/042B64D27/24B64D35/02B64D35/08B64D2221/00Y02T50/44Y02T50/64
    • Rotary-wing aircraft or fixed-wing aircraft consisting of one or a plurality of rotors and/or one or a plurality of airscrews being caused to rotate by means of at least one shaft, the said aircraft comprising a distributed electric motor unit configured to ensure the propulsion and/or the lifting of the said aircraft by causing the said shaft to rotate, the motor unit being a distributed electric motor unit connected directly to the rotating shaft, no mechanism for the transmission of movement being interposed between the said unit and the said shaft, the distributed electric motor unit being composed of a plurality of stacked electric motor elements, each said electric motor element being connected directly to the rotating shaft and consisting of at least one fixed stator and at least one moving rotor capable of connection to the said rotating shaft in order to transmit to it a mechanical power of the following kind where : • Pr = the nominal mechanical power necessary for the propulsion and/or for the lifting of the said aircraft, •Pim = the maximum mechanical power capable of being delivered by the electric motor element on level i, to the rotating shaft, for instance Pim
    • 由一个或多个转子和/或一个或多个螺旋桨组成的旋翼式飞机或固定翼飞机通过至少一个轴被转动,所述飞行器包括分布式电动机单元,其配置成确保 通过使所述轴旋转而使所述飞行器的推进和/或提升,所述马达单元是直接连接到所述旋转轴的分布式电动机单元,所述单元和所述单元之间没有用于传动运动的机构 所述轴,所述分布式电动机单元由多个堆叠的电动机元件组成,每个所述电动机元件直接连接到所述旋转轴,并且包括至少一个固定定子和至少一个能够连接到所述电动机的移动转子 所述旋转轴为了向其传送下列类型的机械功率,其中:°Pr =推荐所需的标称机械功率 lsion和/或用于提升所述飞机,°Pim =能够由电动机元件在等级i上传送到旋转轴的最大机械功率,例如Pim