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1. 发明授权

US4817459A Engine starting and power generating system 失效
标题翻译：发动机起动和发电系统
公开(公告)号：US4817459A
公开(公告)日：1989-04-04
申请号：US137590
申请日：1987-12-24
申请人： Evans W. Erikson , Richard W. Reynolds , Daniel M. Ryan
发明人： Evans W. Erikson , Richard W. Reynolds , Daniel M. Ryan
IPC分类号： F02N11/04 , F16H47/04 , F16H47/00 , F16H47/08
CPC分类号： F02N11/04 , F16H47/04 , F16H2037/0866 , F16H2047/045 , Y10T74/19033
摘要： Operational efficiency in a combined engine starting and power generating system including an engine 110 connected to a dynamoelectric machine 142 useable as a motor or as a generator via a differential 114 and utilizing variable and fixed displacement hydraulic units 146, 156 is increased by sizing the variable and fixed hydraulic units 146 and 156 for power generating operation and by providing an auxiliary fixed displacement hydraulic unit 162 for use only during an engine starting mode.
摘要翻译：组合发动机起动和发电系统的运行效率通过将可变和固定排量液压单元146,156的尺寸调整来增加，该组合发动机起动和发电系统包括连接到电动机142的发动机110，其可用作电动机或作为发电机，通过差速器114和利用可变和固定位移液压单元146,156。和用于发电操作的固定液压单元146和156，并且通过提供仅在发动机起动模式期间使用的辅助固定排量液压单元162。

2. 发明授权

US4908565A Power generating system 失效
标题翻译：发电系统
公开(公告)号：US4908565A
公开(公告)日：1990-03-13
申请号：US15903
申请日：1987-02-18
申请人： Alexander Cook , Richard W. Reynolds
发明人： Alexander Cook , Richard W. Reynolds
IPC分类号： H02J3/38 , H02P9/00 , H02P9/04 , H02P9/08 , H02P9/48
CPC分类号： H02P9/48 , H02P9/08 , H02P2101/30
摘要： A power supply system for developing electrical power from variable-speed motive power produced by a prime mover includes a differential speed summer having a first shaft coupled to the prime mover and further having second and third shafts coupled to first and second generators, respectively, a power conditioner coupled to the second generator for conditioning the power developed thereby and means for regulating the conditioned power developed by the second generator so that the first generator develops constant-frequency AC power.
摘要翻译：用于从由原动机产生的可变速动力来开发电力的电源系统包括差速减速器，其具有联接到原动机的第一轴，并且还具有分别联接到第一和第二发电机的第二和第三轴，耦合到第二发生器的功率调节器，用于调节由此产生的功率，以及用于调节由第二发生器产生的调节功率的装置，使得第一发生器产生恒定的交流电力。

3. 发明授权

US4542722A Combined engine-starter and accessory drive system 失效
标题翻译：发动机起动器和附件驱动系统组合
公开(公告)号：US4542722A
公开(公告)日：1985-09-24
申请号：US562962
申请日：1983-12-19
申请人： Richard W. Reynolds
发明人： Richard W. Reynolds
IPC分类号： F02N7/00 , F02C7/275 , F02C7/32 , F02N15/04 , F02N99/00 , F02N17/00
CPC分类号： F02N15/022 , F02B67/04 , F02N15/04 , F02N11/00 , Y10T74/1926
摘要： An aircraft secondary power system having a selectively operable power source for drive of accessories and for starting of a jet engine. The system includes a clutch which is engaged when the power source is to start the engine. At a predetermined engine speed, the engine takes over the drive of the accessories through the clutch and, at a selected higher speed of the engine, the clutch is disengaged to cause the drive of the accessories from the engine at a lower drive ratio whereby the accessories are driven at a lower speed relative to the speed of the engine.
摘要翻译：具有用于驱动附件和起动喷气发动机的选择性可操作的电源的飞机二次电力系统。该系统包括当电源启动发动机时接合的离合器。在预定的发动机速度下，发动机通过离合器接管附件的驱动，并且在发动机的选定的较高速度下，离合器被分离以使附件从发动机的驱动以较低的驱动比率，由此配件以相对于发动机速度的较低速度被驱动。

4. 发明授权

US4164661A Load sharing system 失效
标题翻译：负载分担系统
公开(公告)号：US4164661A
公开(公告)日：1979-08-14
申请号：US868402
申请日：1978-01-09
申请人： David J. Hucker , Richard W. Reynolds
发明人： David J. Hucker , Richard W. Reynolds
IPC分类号： H02J3/46 , G05B11/32 , H02J1/10 , H02J3/48 , H02J3/04
CPC分类号： H02J1/10 , H02J3/48 , Y10T307/576 , Y10T307/718
摘要： Control systems for controlling load division among plural power sources coupled in parallel and providing power to a common load using feedback techniques. Control systems for various types of plural power sources are disclosed, including DC generators, hydraulic variable displacement pumps and AC generators driven by a constant speed drive. The outputs of the individual power sources are responsive and proportional to individual input control signals. The magnitude of a power component common to all the power sources or frequency, if the power sources are AC generators driven by constant speed drives, is compared to a reference to provide an error signal. Individual sensors sense the magnitude of a variable power component from each power source and provide a signal proportional thereto. Individual signals representing the variable power component are combined with the error signal to provide the individual control signals for each power source.
摘要翻译：用于控制并联耦合的多个电源之间的负载分配的控制系统，并且使用反馈技术向公共负载提供电力。公开了用于各种类型的多个电源的控制系统，包括直流发电机，液压可变排量泵和由恒速驱动器驱动的交流发电机。各个电源的输出响应并与各个输入控制信号成比例。如果电源是由恒速驱动器驱动的交流发电机，则所有电源或频率共同的功率分量的大小与参考值进行比较以提供误差信号。单个传感器感测来自每个电源的可变功率分量的大小并提供与其成比例的信号。表示可变功率分量的各个信号与误差信号组合，以为每个电源提供单独的控制信号。

5. 发明授权

US4882513A Dual permanent magnet generator 失效
标题翻译：双永磁发电机
公开(公告)号：US4882513A
公开(公告)日：1989-11-21
申请号：US812840
申请日：1985-12-23
申请人： Wayne A. Flygare , Raymond N. Olson , Richard W. Reynolds , Mohd A. Aleem
发明人： Wayne A. Flygare , Raymond N. Olson , Richard W. Reynolds , Mohd A. Aleem
IPC分类号： H02K1/20 , H02K16/00 , H02K21/00 , H02K21/14
CPC分类号： H02K21/029 , H02K21/14
摘要： The effects of operational loading on a permanent magnet generator of the type having first and second permanent magnet assemblies 28, 30 mounted on a shaft 26, and movable relative to each other is eliminated by rotatably mounting each of the assemblies 28, 30 for rotation relative to the shaft 26, as well as to each other, and connecting them to the shaft by equal, but oppositely pitched helical spline connections 50, 52, 58, 60. Axial movement of the shaft 26 will then cause equal, but opposite relative movement of the permanent magnet assemblies 28, 30, so that the forces resisting movement of one such assembly act to encourage movement of the other, thereby balancing out said forces.
摘要翻译：通过可旋转地安装每个组件28,30旋转相对于相对于彼此相对移动的具有安装在轴26上并且可相对于彼此移动的第一和第二永久磁铁组件28,30的永久磁铁发生器的操作负载的影响被消除相对于轴26，并且通过相等但相反地倾斜的螺旋花键连接件50,52,58,60将它们连接到轴上，然后轴26的轴向运动将引起相等但相反的相对运动的永磁体组件28,30，使得抵抗一个这样的组件的运动的力作用以促进另一个的运动，从而平衡所述力。

6. 发明授权

US4875403A Variable displacement port plate 失效
标题翻译：可变排量端口板
公开(公告)号：US4875403A
公开(公告)日：1989-10-24
申请号：US259322
申请日：1988-10-18
申请人： Mark S. Stroze , Richard W. Reynolds
发明人： Mark S. Stroze , Richard W. Reynolds
IPC分类号： F03C1/06 , F03C1/253 , F03C1/38 , F03C1/40 , F04B1/20
CPC分类号： F04B1/2042
摘要： An improved hydraulic apparatus is disclosed which may function as either a hydraulic pump or hydraulic motor. A port plate (18) is provided with a high pressure arcuate prot (82) which permits the full range of rotation of the port plate to be used in linearly adjusting the rate of fluid flow into the cylinders (22) of the cylinder block (20). The invention provides a maximum range of adjustability of the volume of fluid flow passing through the cylinders.
摘要翻译：公开了一种改进的液压装置，其可以用作液压泵或液压马达。端口板（18）设置有高压弓形保护件（82），其允许端口板的全部旋转范围用于线性调节流入气缸体的气缸（22）的流体速率（ 20）。本发明提供了通过气缸的流体流量的最大可调整范围。

7. 发明授权

US4077746A Hydraulic intensifier system 失效
标题翻译：液压增压器系统
公开(公告)号：US4077746A
公开(公告)日：1978-03-07
申请号：US460120
申请日：1974-04-11
申请人： Richard W. Reynolds
发明人： Richard W. Reynolds
IPC分类号： F04B1/20 , F15B3/00 , F16H61/40 , F04B17/00 , F16D31/02
CPC分类号： F15B3/00 , F04B1/2042 , F04B2205/063
摘要： A hydraulic intensifier system having an axial piston pump-motor unit with fluid control circuitry associated therewith including porting in the unit whereby hydraulic fluid supplied under pressure to the unit drives the unit, and with part thereof ported to an accumulator for intensification of pressure thereof in an intensify mode of operation. In a start mode, the higher pressure fluid from the accumulator is delivered to the unit to cause rotation of the unit in an opposite direction.
摘要翻译：一种液压增压器系统，其具有轴向活塞泵 - 马达单元，其具有与其相关联的流体控制电路，包括在单元中的移入，其中在压力下供应到该单元的液压流体驱动该单元，并且其一部分移入蓄能器以增强其压力强化操作模式。在启动模式下，来自蓄能器的较高压力的流体被输送到单元以使单元沿相反方向旋转。

8. 发明授权

US5014507A Direct drive gaseous hydrogen turbo actuator 失效
标题翻译：直接驱动气态氢气涡轮致动器
公开(公告)号：US5014507A
公开(公告)日：1991-05-14
申请号：US450531
申请日：1989-12-14
申请人： John N. Rice , Richard W. Reynolds
发明人： John N. Rice , Richard W. Reynolds
IPC分类号： F02K9/56
CPC分类号： F02K9/56 , Y10T137/87338
摘要： A propulsion engine (12) which combusts propellant received from the storage tank (24) in which a portion (28) of the tank contains propellant in the liquid state and in which an ullage (26) in a remaining portion of the tank contains the propellant in a gaseous state including a first propellant circuit (34) coupling liquid propellant stored in the tank to an evaporator (30); a second propellant circuit (36), coupling the gaseous propellant from the evaporator to the propulsion engine combustor and to the ullage; at least one power generating device (14 and 16) disposed in the second propellant circuit between the evaporator and the ullage, for providing a power output from energy of the gaseous propellant flowing in the second propellant circuit controlled by at least one control valve controlling a flow of gaseous propellant to the at least one device under the control of at least one valve control signal; a bypass circuit (40) coupled in parallel with the at least one power generating device containing a bypass valve (42) controlling flow of gaseous propellant through the bypass circuit from the evaporator to the ullage in response to a bypass valve control signal; and a controller (44) coupled to the bypass valve and the at least one control valve, for generating the valve control signal controlling the flow of gaseous propellant through the valves to produce a controlled mass flow of gaseous propellant into the ullage independent of variation of a mass of gas flow through the valves.
摘要翻译：燃料从储罐（24）接收的推进剂的推进发动机（12），其中罐的一部分（28）包含处于液体状态的推进剂，并且其中罐的剩余部分中的空气（26）包含包括将存储在罐中的液体推进剂与蒸发器连接的第一推进剂回路（34）的气态的推进剂; 第二推进剂回路（36），将气体推进剂从蒸发器耦合到推进发动机燃烧器并且连接到空缺; 设置在所述第二推进剂回路中的至少一个发电装置（14和16），位于所述蒸发器和所述空调之间，用于从由所述第二推进剂回路中流动的气体推进剂的能量提供功率输出，所述第二推进剂回路由至少一个控制阀在至少一个阀门控制信号的控制下，气体推进剂流到至少一个装置; 旁路回路（40），其与所述至少一个发电装置并联连接，所述旁路回路（40）包含旁路阀（42），所述旁路阀（42）响应于旁通阀控制信号控制通过所述旁通回路从所述蒸发器到所述空置的气体推进剂的流动; 以及联接到所述旁通阀和所述至少一个控制阀的控制器（44），用于产生阀控制信号，所述阀控制信号通过所述阀来控制气体推进剂的流动，以产生气体推进剂受控的质量流量，大量气体流过阀门。

9. 发明授权

US4557160A Hydraulic differential transmission 失效
标题翻译：液压差速传动
公开(公告)号：US4557160A
公开(公告)日：1985-12-10
申请号：US642078
申请日：1984-08-20
申请人： Richard W. Reynolds
发明人： Richard W. Reynolds
IPC分类号： F16H47/04
CPC分类号： F16H47/04 , F16H2037/0873
摘要： A hydraulic differential transmission utilizing an input differential and having a hydrostatic transmission with a variable output speed to the input differential whereby the speed of the transmission drive output can be maintained constant with variable drive input speeds to the transmission. The hydraulic differential transmission has a pair of parallel drive trains between the drive shaft of the fixed displacement unit of the hydrostatic transmission and the input differential, with the two drive trains providing different drive ratios therebetween. A first drive train including an overrunning clutch provides a one to one drive ratio therebetween when operating at higher drive input speeds. The other drive train includes a second differential and a second overriding clutch providing a lesser drive ratio between the fixed displacement hydraulic unit and the first differential when operating at lower drive input speeds. The overrunning clutches enable a shift between drive trains at a shift point where the drive shaft of the fixed displacement hydaulic unit changes direction of rotation without any discontinuity in the drive at the shift point. The change in drive ratios for operation at the higher drive input speeds causes the hydraulic units of the hydrostatic transmission to operate at higher pressures and nearer their normal pressure capabilities.
摘要翻译：一种利用输入差速器并具有可变输出速度的输入差速器的液压差速传动装置的液压差速传动装置，由此传动驱动输出的速度能够以变速器的可变驱动输入速度保持恒定。液压差速变速器在静液压变速器的固定排量单元的驱动轴和输入差速器之间具有一对平行的传动系，两个传动系在它们之间提供不同的传动比。当在较高的驱动输入速度下运行时，包括超越离合器的第一传动系提供一对一的驱动比。另一传动系包括第二差速器和第二超控离合器，当以较低的驱动输入速度运行时，该固定离合器提供固定位移液压单元与第一差速器之间较小的驱动比。超越离合器使得在固定位移液压单元的驱动轴改变转动方向的换档点处的驱动系之间的移动，而在换档点处的驱动器中没有任何不连续性。在较高的驱动输入速度下操作的驱动比的变化导致静液压传动的液压单元在更高的压力下操作并且接近它们的正常压力能力。

10. 发明授权

US4217120A Air-oil separator for aircraft gearbox 失效
标题翻译：飞机齿轮箱用空气分离器
公开(公告)号：US4217120A
公开(公告)日：1980-08-12
申请号：US844014
申请日：1977-10-20
申请人： Richard W. Reynolds
发明人： Richard W. Reynolds
IPC分类号： F16K24/04 , B04B1/02 , B64D33/00 , F01M13/04 , F16H57/027 , F16N7/36 , B01D50/00
CPC分类号： F16H57/04 , B64D33/00 , F16H57/027 , F16N7/36 , F01M2013/0422 , F16N2210/02
摘要： In a gearbox for an aircraft, a multiple stage separator is attached to a gear journaled within the gearbox housing. An axial bore extends at least partially through the shaft supporting the gear and opens into a discharge chamber which communicates with an atmospheric vent. A first stage of the separator includes an impeller attached to one face of the gear and a second stage includes a series of angularly spaced passages extending in a generally radial direction through the shaft to communicate with the bore. A sleeve telescoped into a reduced section of the inner end of the bore receives the incoming mixture of air and oil and directs the air into an enlarged outer end section of the bore wherein final stage separation of air and oil occurs. A member including an aperture concentric with the central axis of the bore keeps the oil collected along the walls of the bore from entering into the discharge chamber. A passage defined by a flat formed on the outside of the sleeve provides a flow path in a direction away from the discharge chamber for the collected oil to exit the bore back to the interior of the housing.
摘要翻译：在用于飞机的变速箱中，多级分离器附接到齿轮箱壳体内的齿轮。轴向孔径至少部分延伸穿过支撑齿轮的轴并且通向与大气通气口连通的排放室。分离器的第一级包括附接到齿轮的一个表面的叶轮，并且第二级包括一系列角度间隔的通道，该通道在大致径向方向上延伸穿过轴以与孔连通。可伸缩到孔的内端的减少部分的套筒容纳空气和油的进入混合物，并将空气引导到孔的扩大的外端部分，其中发生空气和油的最后阶段分离。包括与孔的中心轴线同心的孔的构件保持沿着孔的壁收集的油进入排放室。由形成在套筒外部的平坦部限定的通道在远离排放室的方向上提供流动路径，以使收集的油离开孔返回到壳体的内部。

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