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1. 发明授权

US4695736A Variable speed wind turbine 失效
标题翻译：变速风力发电机
公开(公告)号：US4695736A
公开(公告)日：1987-09-22
申请号：US799045
申请日：1985-11-18
申请人： Glidden S. Doman , Joseph M. Kos , Kermit I. Harner , Eugene D. DiValentin , Henry S. Healy
发明人： Glidden S. Doman , Joseph M. Kos , Kermit I. Harner , Eugene D. DiValentin , Henry S. Healy
IPC分类号： F03D7/04 , F03D7/02 , F03D9/00 , H02P9/42 , F03D9/02
CPC分类号： H02P9/42 , F03D7/0272 , F03D9/003 , F05B2220/706 , F05B2260/96 , F05B2270/101 , F05B2270/1016 , F05B2270/1032 , F05B2270/20 , F05B2270/327 , H02P2101/15 , Y02E10/723 , Y02E10/725
摘要： A variable speed wind turbine includes a frequency converter which converts variable frequency AC from a turbine driven AC generator to fixed frequency AC for delivery to a power grid. The frequency converter is typically an electronic cycloconverter or rectifier-inverter and is also used to control the power flow from the AC generator to the grid which thereby controls the air gap torque between the generator stator and rotor. The turbine speed is maneuvered to increase efficiency by precisely controlling the air gap torque according to a schedule defining sensed generator speed versus sensed generated power.
摘要翻译：变速风力涡轮机包括变频器，该变频器将来自涡轮驱动的交流发电机的可变频率AC转换成固定频率的交流电，用于输送到电网。变频器通常是电子循环换流器或整流器逆变器，并且还用于控制从AC发电机到电网的功率流，从而控制发电机定子和转子之间的气隙扭矩。通过根据定义感测的发电机速度与感测的发电功率的调度精确地控制气隙转矩来操纵涡轮机速度以提高效率。

2. 发明授权

US4353681A Wind turbine with yaw trimming 失效
标题翻译：具有偏航修整的风力涡轮机
公开(公告)号：US4353681A
公开(公告)日：1982-10-12
申请号：US151016
申请日：1980-05-19
申请人： Glidden S. Doman
发明人： Glidden S. Doman
IPC分类号： F03D7/04 , F03D1/00 , F03D7/02
CPC分类号： F03D1/00 , F03D7/0204 , Y02E10/721 , Y02E10/723
摘要： Yaw trimming in large wind turbines is achieved by laterally offsetting the turbine yaw axis from the axis of rotation of the hub.
摘要翻译：在大型风力涡轮机中的偏航修剪是通过将涡轮偏航轴线从轮毂的旋转轴线横向偏移来实现的。

3. 发明授权

US4329117A Wind turbine with drive train disturbance isolation 失效
标题翻译：风力发电机组与传动系干扰隔离
公开(公告)号：US4329117A
公开(公告)日：1982-05-11
申请号：US142783
申请日：1980-04-22
申请人： Glidden S. Doman
发明人： Glidden S. Doman
IPC分类号： F03D7/04 , F03D7/02 , F03D15/00 , F03D11/02
CPC分类号： F03D15/00 , F05B2270/20 , Y02E10/723 , Y10S416/50
摘要： A wind turbine adapted to rotationally drive a load such as an electric power generator 50 includes in the turbine drive train, resiliently mounted gearing 55 which isolates and damps the load from drive train disturbances caused by wind gusts and wind stream dyssemmetry and inherent torsional vibration without assistance from modulation of turbine blade pitch.
摘要翻译：适于旋转地驱动诸如发电机50的负载的风力涡轮机包括在涡轮传动系中，弹性安装的传动装置55，其将负载与由阵风引起的传动系扰动和风流不稳定性以及固有的扭转振动隔离并且阻止负载，而没有协助调整涡轮叶片间距。

4. 发明授权

US4073600A Damping mechanism for the rotor hub of a helicopter for ground resonance and waddle and its combination with the rotor 失效
标题翻译：用于地面共振和桨叶的直升机转子轮毂的阻尼机构及其与转子的组合
公开(公告)号：US4073600A
公开(公告)日：1978-02-14
申请号：US695737
申请日：1976-06-14
申请人： Glidden S. Doman
发明人： Glidden S. Doman
IPC分类号： B64C27/00 , B64C27/41 , B64C27/52
CPC分类号： B64C27/41 , B64C27/001 , B64C2027/002
摘要： A damping mechanism is disclosed for damping the oscillations of the rotor hub which are coupled with periodic motions of the fuselage when on the ground, known as ground resonance, and a waddle when in the air. The rotor includes a freely tiltable rotor head mounted on a non-rotatable universal joint having an outer gimbal ring and an inner ring carried by a pylon. The damping mechanism connected between a gimbal ring and the pylon combines the action of a fluid dashpot in tandem with spring means the output of which is connected into the linkage between the pilot stick and the swash plate. The tandem combination of dash pot and spring means delays the signal to the swash plate by about 90.degree. to insert a corrective movement into the swash plate with feathering of the blades to tilt the rotor thrust vector which damps the oscillations of the rotor hub. The invention includes the damping mechanism per se and its combination with the rotor and with the swash plate.
摘要翻译：公开了一种用于阻尼转子毂的振荡的阻尼机构，其在地面上与机身的周期性运动相耦合，称为地面共振，以及在空气中时的瓦鞍。该转子包括一个可自由倾斜的转子头，该转子头安装在一个非旋转的万向接头上，该万向节具有外部万向节环和一个由塔架承载的内圈。连接在万向环和吊架之间的阻尼机构将流体缓冲器的作用与弹簧装置结合，弹簧装置的输出连接到导向杆和斜盘之间的连杆中。仪表盘和弹簧的串联组合意味着将信号延迟到斜盘约90°，以将叶片的羽化将旋转斜盘插入旋转斜盘，使转子推力矢量倾斜，从而减小转子毂的振荡。本发明包括阻尼机构本身及其与转子和斜盘的组合。

5. 发明授权

US4515525A Minimization of the effects of yaw oscillations in wind turbines 失效
标题翻译：最小化风力发电机中偏航振荡的影响
公开(公告)号：US4515525A
公开(公告)日：1985-05-07
申请号：US440056
申请日：1982-11-08
申请人： Glidden S. Doman
发明人： Glidden S. Doman
IPC分类号： F03D7/04 , F03D7/02 , F15B11/08
CPC分类号： F03D7/0204 , Y02E10/723 , Y10S416/06 , Y10S416/50
摘要： Yaw (fishtail) oscillations in large wind turbines (10) are minimized by damping provided by a drive motor (65) connecting the turbine to the supporting tower (50) therefor at, for example, a yaw bearing (45). The drive motor drives the wind turbine in yaw and maintains desired yaw settings of the turbine. The motor is also capable of being driven by yaw oscillations of the wind turbine and in being so driven, dissipates the energy of such oscillations.
摘要翻译：在大型风力涡轮机（10）中的偏航（鱼尾）振荡通过将涡轮连接到例如偏航轴承（45）的支撑塔（50）的驱动马达（65）提供的阻尼来最小化。驱动马达驱动风力涡轮机偏航并维持涡轮机的所需偏航设置。电动机还能够被风力涡轮机的偏航振荡驱动，并且在被驱动的情况下消散这种振荡的能量。

6. 发明授权

US4004757A Oscillation damper for the hub of a rotorcraft rotor and its combination with a rotorcraft 失效
标题翻译：旋翼飞轮转子的轮毂振动阻尼器及其与旋翼航空器的组合
公开(公告)号：US4004757A
公开(公告)日：1977-01-25
申请号：US623008
申请日：1975-10-16
申请人： Glidden S. Doman
发明人： Glidden S. Doman
IPC分类号： B64C27/58 , B64C11/44
CPC分类号： B64C27/58 , Y10S416/50
摘要： A rotorcraft is subject to a rocking motion when on the ground, which is called ground resonance, and in the air which gives the fuselage a waddle type of motion about its center of gravity. both are a form of aeromechanical instability. This fuselage motion is coupled with and accompanied by bending oscillations of the blades with respect to the hub of the rotor of the rotorcraft. An oscillation damper is described which damps the oscillations of the aircraft and thereby eliminates or substantially reduces the rocking and waddle motion of the fuselage. The damper includes a seismic device having a mass-spring combination tuned to the frequency of the rocking motion which will typically be one half or approximately one half of the rotor revolutions per minute at cruising speed and is positioned laterally of and spaced from the center of gravity of the fuselage. The movement of the weight in response to fuselage motion operates a control and the control operates a motor which expands and contracts in response thereto. The motor is connected with the swash plate to change the pitch of the blades of the rotor in proper phase relation with the hub oscillation and thereby provide a vector force which damps the oscillations. The control particularly illustrated is a pair of fluid valves and the motor is a fluid motor.
摘要翻译：旋翼航空器在地面上受到摇摆运动，称为地面共振，并且在空气中使机身围绕其重心产生鞍形运动。两者都是一种航空力学不稳定的形式。该机身运动与叶片相对于旋翼飞机的转子的轮毂的弯曲振荡相耦合并伴随着弯曲振荡。描述了一种减振飞行器振荡的振动阻尼器，从而消除或基本上减少了机身的摇摆和瓦楞运动。阻尼器包括具有调整到摇摆运动频率的质量 - 弹簧组合的地震装置，其通常将以每分钟的巡航速度的转子转数的一半或大约一半定位并且位于机身重力。响应于机身运动的重量的运动进行控制，并且控制操作电动机，其响应于此而增大和收缩。电动机与斜盘连接，以改变转子叶片的桨距与轮毂振荡的正确相位关系，从而提供阻止振荡的矢量力。具体示出的控制是一对流体阀，电机是流体马达。

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