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    • 3. 发明公开
    • Limited angle torque motor
    • 伺服电机具有有限的角运动。
    • EP0160132A1
    • 1985-11-06
    • EP84302746.7
    • 1984-04-24
    • Pneumo Abex Corporation
    • Vanderlaan, Robert D.Meulendyk, John W.
    • H02K26/00H02K5/128
    • H01F7/145H02K5/1285H02K26/00
    • A two pole stationary coil rotary magnet motor (1) which provides for increased work and reduced rotary inertia. The motor consists of two main assemblies, a rotor assembly (2) contained within a rotor casing (3) and a stator and housing assembly (4) surrounding the rotor casing. One end of the casing is closed, whereas the other end is open to eliminate the need for a dynamic shaft seal. Fluid enters the casing at the open end (12) thereof to provide a lubricating fluid for the rotor bearings (7, 8) and a heat conductive path. The rotor casing isolates the critical movement of the rotor (6) from the contaminated atmosphere of the stator environment and allows replacement of the stator assembly (4) without disturbing the rotor assembly. A permanent magnet rotor (6) may be formed using one or more rare earth magnets (45) which may be suitably bonded to the rotor shaft. A protective cover (49) surrounds the rotor magnets to eliminate potential rotor magnet breakage contamination. The relationship between the rotor magnet angle and stator winding (40, 41) may be such as to produce a relatively large output work potential. Also, the lamination slot configuration and stator winding may be graded to optimize the torque versus rotation profile to more closely match the cosine function of various rotary to linear output gearing to provide a substantially constant force output.
    • 4. 发明公开
    • Opposed piston type free piston engine pump unit
    • Einheit aus Freikolbenmotor und Pumpe。
    • EP0085800A2
    • 1983-08-17
    • EP82300655.6
    • 1982-02-10
    • Pneumo Abex Corporation
    • Vanderlaan, Robert D.
    • F04B17/00F04B49/00
    • F04B17/05
    • A free piston engine pump converts combustion energy into hydraulic power in an efficient, controlled and relatively uncomplicated manner, for example, for vehicle propulsion, auxiliary system power, etc. The free piston engine pump is substantially naturally mass balanced having opposed engine pistons 5, driving respective in-line hydraulic pumps 3. An adjustable accumulator 49 with a deformable fluid-tight chamber 50 containing a compressible fluid stores and delivers energy for compression, and an arrangement of control valves 67-69 and check valves 62, 63, 65, 66 enables selective operation of the free piston engine pump in primary (high flow) and secondary (high pressure) modes. Plural free piston engine pumps la, 1b, may be interfaced for parallel operation sharing common elements 53', 64' and functions. Cycle rate, intermittent operation and start-up also may be controlled. Electronic monitoring and control 150 of one or more operational parameters of a free piston engine pump also are disclosed.
    • 自由活塞发动机泵以高效,受控和相对简单的方式将燃烧能量转换为液压动力,例如用于车辆推进,辅助系统动力等。自由活塞发动机泵基本上是天然的质量平衡的,具有相对的发动机活塞5, 驱动相应的在线液压泵3.具有包含可压缩流体的可变形流体密封室50的可调累积器49存储并输送用于压缩的能量,并且配置控制阀67-69和止回阀62,63,65 66允许在初级(高流量)和次级(高压)模式中选择性地操作自由活塞式发动机泵。 多个自由活塞式发动机泵1a,1b可以被接口用于并行操作共同共同的元件53分钟,64分钟和功能。 循环速率,间歇操作和启动也可以被控制。 还公开了一种自由活塞式发动机泵的一个或多个操作参数的电子监视和控制150。
    • 7. 发明公开
    • Control actuation system including staged direct drive valve with fault control
    • Kontrollbetätigungssystenmit direkt angetriebenem Stufenventil und Fehlerkontrolle。
    • EP0115925A1
    • 1984-08-15
    • EP84300329.4
    • 1984-01-19
    • Pneumo Abex Corporation
    • Vanderlaan, Robert D.
    • F15B18/00
    • F15B18/00
    • A control actuation system (70) for an aircraft including an electro-mechanically controlled, hydraulically powered actuator (72) for driving a main control valve (26) of a dual hydraulic servo-actuator control system (10). The actuator includes a tandem piston (74) connected to the main control valve (26) which is controllably positioned by a staged valve (125) of relatively short stroke whereby a force motor (218) of minimum size and energy requirements may be used to directly drive the valve. The staged valve (125) includes a linearly movable valve plunger (184) for simultaneously controlling the differential application of fluid pressure from respective hydraulic system on opposed pressure surfaces (94, 96 and 98, 100) of respective piston sections (90, 92) to cause movement of the piston (74) in response to relatively short axial movement of the valve plunger as long as at least one hydraulic system remains operative. Also, the staged valve (125) includes a fault control valve sleeve (130) concentric with the valve plunger (184) which, upon shut-down or failure of both hydraulic systems, moves linearly to render the valve plunger inoperative and release fluid pressure from opposed, corresponding pressure surfaces (94, 96 and 98, 100) of the tandem piston to respective returns therefor through respective centering rate control orifices (118,120, 250, 252) in the fault control valve sleeve (130) as the piston in moved to a neutral position by a centering spring device (254) acting on the main control valve.
    • 一种用于飞行器的控制致动系统(70),其包括用于驱动双液压伺服致动器控制系统(10)的主控制阀(26)的电机械控制的液压动力致动器(72)。 致动器包括连接到主控制阀(26)的串联活塞(74),其通过相对较短行程的分级阀(125)可控地定位,由此可以使用最小尺寸和能量要求的力马达(218)来 直接驱动阀门。 分级阀125包括可直线运动的阀柱塞184,用于同时控制相应的液压系统在相应的活塞部分(90,92)的相对的压力表面(94,96和98,100)上差动地施加流体压力, 以便只要至少一个液压系统保持工作,响应于阀柱塞的相对短的轴向运动而引起活塞(74)的移动。 此外,分级阀125还包括与阀柱塞184同心的故障控制阀套管130,在两个液压系统关闭或故障时,该活塞阀线性移动,使得阀柱塞不起作用并释放流体压力 通过作为活塞的故障控制阀套(130)中的相应的对中速度控制孔(118,120,250,252),从串联活塞的相对的相应的压力表面(94,96和98,100)到相应的回程, 通过作用在主控制阀上的定心弹簧装置(254)移动到中立位置。
    • 10. 发明公开
    • Torque motor with high torque poles and magnetic centering spring adjustment
    • 扭矩与高转矩和磁极由弹簧调整定心。
    • EP0187038A2
    • 1986-07-09
    • EP85309435.7
    • 1985-12-23
    • Pneumo Abex Corporation
    • Vanderlaan, Robert D.Eiszner, William H., Jr.
    • H02K26/00
    • H01F7/145H02K26/00
    • A two-pole limited angle torque motor (1) including a rotor assembly (2) having one or more permanent rotor magnets (5) and a stator assembly (6) including a stator coil (9) and a pair of circumferentially spaced stator pole structures (10, 11). Each pole structure (10, 11) includes a generally axially extending stator pole blade (14) about which the stator coil (9) circumferentially extends. A radially outwardly extending flange (15) is at one end of one of the stator pole structures (10) and at the opposite end of the other stator pole structure (11). The stator pole blades (14) have a greater radial thickness (20) adjacent the flanges thereof than at the opposite end of the blade to reduce the magnetic flux density of the stator pole structures in the region of the blades adjacent the flanges thereof. Also, the axial outer end faces (21) of the flanges (15) desirably protrude axially outwardly adjacent the radial inner ends thereof to make use of the fringing fields of the rotor magnet at the ends of the rotor assembly to increase the reluctance torque of the motor. At the ends of the stator assembly (9) opposite the stator pole flanges (15) on opposite sides of the rotor assembly (2) are additional stator pole pieces (24). The blades (14) of the stator pole structures (10, 11) terminate short of the other ends of the rotor magnet (5) to provide room for the additional stator pole pieces (24) at such other ends for a given rotor length whereby the motor has a substantially higher reluctance torque without significantly reducing the torque due to interaction of magnetic fields. Surrounding the stator assembly in an outer magnetic housing (16) comprising two semi-cylindrical parts (30, 31) with air gaps (17, 18) between opposite sides thereof, said housing parts being rotatable relative to each other to change the size of one gap relative to the other or otherwise machinable to change both gaps equally for adjusting the reluctance torque of the motor.