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    • 21. 发明授权
    • Bidirectional dual disc valve assembly
    • 双向双盘阀组件
    • US4972929A
    • 1990-11-27
    • US362798
    • 1989-06-07
    • Douglas E. IversLeonard J. Schwemmer
    • Douglas E. IversLeonard J. Schwemmer
    • F16F9/348
    • F16F9/3484
    • The bidirectional valve assembly provides for selection of retraction and extension damping characteristics which can accommodate relatively large separation of damping curves. Two cooperable valve discs or ring members are provided which function in unison to resist fluid flow in a first fluid flow direction, while a single one of the valve ring members functions primarily to resist fluid flow in the other direction. In a first embodiment, one of the two cooperable valve ring members comprises a compliant retainer or fulcrum against which the other valve ring member moves in unison therewith to produce relatively low damping in retraction. The other valve ring member moves alone in extension to produce relatively high damping. In an alternative embodiment, the two cooperable valve ring members are superimposed and move in unison during extension, as dictated by their combined stiffness. In retraction, fluid passes through openings in one of the valve ring members for contact with and movement of the other, relatively compliant valve ring member.
    • 双向阀组件提供了可以适应相对大的阻尼曲线分离的回缩和延伸阻尼特性的选择。 提供两个配合的阀盘或环构件,其一致地起着抵抗第一流体流动方向上的流体流动的作用,同时单个阀环构件主要用于抵抗另一个方向上的流体流动。 在第一实施例中,两个可协调的阀环构件中的一个包括顺应的保持器或支点,另一个阀环构件与其一起移动以与其一起移动以在缩回中产生相对较低的阻尼。 另一个阀环构件在延伸中单独移动以产生相对较高的阻尼。 在替代实施例中,两个可配合的阀环构件被叠加并在延伸期间一致地移动,如其组合的刚度所规定的。 在回缩时,流体通过一个阀环构件中的开口,用于与另一个相对顺应的阀环构件接触和移动。
    • 24. 发明授权
    • Efficient multi-directional active vibration absorber assembly
    • 高效多方向主动减震器总成
    • US6009985A
    • 2000-01-04
    • US799065
    • 1997-02-10
    • Douglas E. Ivers
    • Douglas E. Ivers
    • F16F7/10F16F7/104
    • F16F7/1005F16F7/104F16F2224/0283
    • An Active Vibration Absorber assembly (20) including a casing (24), a first tuning mass (32) supported relative to the casing (24) which is actively vibratable by a force generator (40) in a first direction (along an A--A axis), a second tuning mass (32') supported relative to said casing (24) which is actively vibratable by a force generator (40') in a second direction (along axis B--B) generally orthogonal to the first direction, and a flexible member (26) flexibly supporting the casing (24). In a first embodiment, the tuning masses (32, 32') are vibratable by a magnet and coil assembly within shakers (25, 25') and the flexible member (26) is a beam. In other embodiments, multiple beams are employed to restrict the vibration of casing (24) to substantially planar motion. The AVA assembly (20) finds application in Active Structural Control (ASC) systems for actively canceling vibration or noise in vehicle cabins (example: automobiles, aircraft).
    • 一种主动减振器组件(20),包括壳体(24),相对于壳体(24)支撑的第一调谐质量块(32),所述第一调谐质量块(32)可通过力产生器(40)在第一方向(沿着AA轴线) ),相对于所述壳体(24)支撑的第二调谐质量块(32'),所述第二调谐质量块(32')在大致垂直于所述第一方向的第二方向(沿着轴线BB))上由力发生器(40')可主动振动,以及柔性构件 (26)柔性地支撑壳体(24)。 在第一实施例中,调谐质量块(32,32')可由振动器(25,25')内的磁体和线圈组件振动,并且柔性构件(26)是梁。 在其他实施例中,采用多个梁来将壳体(24)的振动限制为基本上平面的运动。 AVA组件(20)在主动结构控制(ASC)系统中应用,主动消除车厢内的振动或噪音(例如:汽车,飞机)。
    • 25. 发明授权
    • Active structural control system and method including active vibration
absorbers (AVAS)
    • 主动结构控制系统和方法包括主动减振器(AVAS)
    • US6002778A
    • 1999-12-14
    • US693742
    • 1996-08-07
    • Dino J. RossettiDouglas E. IversMark A. NorrisMichael C. HeathSteve C. Southward
    • Dino J. RossettiDouglas E. IversMark A. NorrisMichael C. HeathSteve C. Southward
    • G10K11/178A61F11/06
    • G10K11/1786G10K2210/121G10K2210/1281G10K2210/129G10K2210/3026G10K2210/3027G10K2210/3051G10K2210/3211G10K2210/501
    • An Active Structural Control (ASC) system (10) and method which includes a plurality of Active Vibration Absorbers (AVAs) (40) attached to a yoke (32) included within a pylon structure (28) preferably comprising a spar (38) and a yoke (32) which is located intermediate between an aircraft fuselage (20) and an aircraft engine (18) for controlling acoustic noise and/or vibration generated within the aircraft's cabin (44) due to unbalances in the aircraft engine (18). The ASC system (10) includes a plurality of error sensors (42) for providing error signals, and at least one reference sensor (49 or 50) for providing reference signals indicative of the N1 and/or N2 engine rotations and/or vibrations, and a preferably digital electronic controller (46) for processing the error and reference signal information to provide output signals to drive the plurality of AVAs (40) attached to the yoke (32). The AVAs (40) preferably act in a radial, tangential, or fore and aft directions and may be preferably located at the terminal end and/or at the base portion of the yoke (32). Further, the AVAs (40) may be Single Degree Of Freedom (SDOF) or Multiple Degree Of Freedom (MDOF) and may be tuned to have a passive resonance which substantially coincides with the N1 and/or N2 engine rotation and/or vibrations. In another aspect, reference signal processing is described which includes a modulo counter, a lookup table, and a digital IO.
    • 一种主动结构控制(ASC)系统(10)和方法,其包括附接到包括在塔架结构(28)内的轭架(32)的多个主动减振器(AVAs)(40),优选地包括翼梁(38)和 位于飞行器机身(20)和飞机发动机(18)之间的轭架(32),用于控制由于飞行器发动机(18)中的不平衡而在飞机机舱(44)内产生的声音噪声和/或振动。 ASC系统(10)包括用于提供误差信号的多个误差传感器(42)和用于提供指示N1和/或N2发动机转动和/或振动的参考信号的至少一个参考传感器(49或50) 以及用于处理误差和参考信号信息以提供输出信号以驱动附接到磁轭(32)的多个AVA(40)的优选数字电子控制器(46)。 AVA(40)优选地以径向,切向或前后方向作用,并且可以优选地位于轭架(32)的终端和/或基座部分处。 此外,AVA(40)可以是单自由度(SDOF)或多自由度(MDOF),并且可以被调谐为具有与N1和/或N2发动机旋转和/或振动基本一致的无源共振。 在另一方面,描述了包括模计数器,查找表和数字IO的参考信号处理。
    • 27. 发明授权
    • Semi-active damper valve means with electromagnetically movable discs in
the piston
    • 半主动阻尼阀装置,在活塞中具有电磁可移动盘
    • US4921272A
    • 1990-05-01
    • US310145
    • 1989-02-10
    • Douglas E. Ivers
    • Douglas E. Ivers
    • B60G17/08F16F9/46F16F9/516
    • B60G17/08F16F9/46F16F9/516B60G2202/24B60G2400/102B60G2400/202B60G2400/252B60G2500/10B60G2600/184B60G2800/012B60G2800/24B60G2800/912
    • An improved method and means for control and accomplishment of semi-active damper means transition between high damping and low damping states is provided which takes advantage of the available inherent dynamic fluid pressure forces produced by the condition of motion between supported and supporting members. Deferral or delay of damper state transitions to avoid force discontinuities or system noise is accomplished mechanically, or automatically internal to the structure of the adjustable valve means. The delay of damper state transition from high to low and low to high damping is accomplished independent of the particular control policy utilized until the fluid pressure differential across the valve ring members is a preselected low value. Commanded valve switching and motion condition sensing requirements are also minimized by reversible check valve means. Damper state transitions normally required based on a sign change in relative velocity are accomplished without actuated change in valve ring position by one of the inner and outer valve rings (in the "off" state) which floats between flow permitting and flow restricting positions dependent upon the direction of fluid flow through the piston.
    • 提供了一种用于控制和实现半主动阻尼器的改进方法和装置,其在高阻尼和低阻尼状态之间的过渡,其利用由支撑构件和支撑构件之间的运动状态产生的可用的固有动态流体压力。 缓冲器状态转换的延迟或延迟以避免力中断或系统噪声机械地实现,或者在可调节阀装置的结构内部自动实现。 阻尼器状态从高到低和高阻尼转变的延迟是独立于所使用的特定控制策略而实现的,直到阀环构件上的流体压力差是预选的低值。 指令阀切换和运动状态检测要求也通过可逆止回阀装置最小化。 基于相对速度的符号变化通常需要的阻尼器状态转换通过内阀和外阀之间的一个(处于“关”状态)而在阀环位置上的动作变化下实现,该阀环位于依赖于流动允许和限流位置之间浮动 流体流过活塞的方向。