会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 8. 发明授权
    • Hydraulic regeneration system
    • 液压再生系统
    • US07444809B2
    • 2008-11-04
    • US11341630
    • 2006-01-30
    • David P. SmithDaniel T. Mather
    • David P. SmithDaniel T. Mather
    • F16D31/02
    • F15B21/14E02F9/2217E02F9/2292F15B11/006F15B2211/20523F15B2211/30575F15B2211/625F15B2211/7053F15B2211/88
    • A hydraulic system for a work machine is provided. The hydraulic regeneration system has a tank, a primary source, a first actuator, an accumulator, and a first valve mechanism. The tank is configured to hold a supply of fluid. The primary source is configured to pressurize the fluid and has a suction inlet and a discharge outlet. The first actuator is configured to receive pressurized fluid from the discharge outlet of the primary source. The accumulator is in fluid communication with the tank, the suction inlet of the primary source, and the first actuator. The first valve mechanism is disposed between the suction inlet of the primary source and the accumulator, and is movable between a first position at which fluid returning from the first actuator is directed to the suction inlet of the primary source, and a second position at which fluid returning from the first actuator is directed to only the accumulator.
    • 提供了一种用于作业机械的液压系统。 液压再生系统具有罐,主源,第一致动器,蓄能器和第一阀机构。 罐被配置成保持流体供应。 主要来源被配置为对流体加压并具有吸入口和排出口。 第一致动器构造成从主源的排出口接收加压流体。 蓄能器与罐,主源的吸入口和第一致动器流体连通。 第一阀机构设置在主源的吸入口和蓄能器之间,并且可在第一位置和第二位置之间移动,在第一位置,第一位置和第二位置之间,第一位置使从第一致动器返回的流体被引导到主源的吸入口, 从第一致动器返回的流体仅被引导到蓄能器。
    • 9. 发明授权
    • High force feel bumper with low final load
    • 高力感觉保险杠与最终负载低
    • US06394431B1
    • 2002-05-28
    • US09813539
    • 2001-03-21
    • David P. Smith
    • David P. Smith
    • G05G506
    • G05G5/03F16H61/24G05G2009/04766Y10T74/20201Y10T74/20612
    • The feel bumper includes a plunger disposed for movement by an input device along a predetermined path, and at least one damper element disposed to engage the plunger when in a predetermined initial position along the path corresponding to a desired operating position for exerting a first opposing feedback force against the plunger in opposition to movement thereof along the path in a first direction, the at least one damper element being yieldable to the plunger when moved in the first direction past the predetermined initial position and exerting a second opposing feedback force against the plunger in opposition to the continued movement of the plunger in the first direction through subsequent operating positions.
    • 感觉保险杠包括设置成沿着预定路径由输入装置移动的柱塞,以及设置成当沿着对应于期望操作位置的路径处于预定初始位置时接合柱塞的至少一个阻尼器元件用于施加第一相对反馈 所述至少一个阻尼器元件在所述第一方向上移动超过所述预定的初始位置并且向所述柱塞施加相对于所述柱塞的第二相对的反作用力时可屈服于所述柱塞 与柱塞在第一方向上通过后续操作位置的持续移动相反。
    • 10. 发明授权
    • Countermeasure apparatus for deploying interceptor elements from a spin stabilized rocket
    • 用于从自旋稳定火箭部署拦截器元件的对策装置
    • US06279482B1
    • 2001-08-28
    • US08961900
    • 1997-10-31
    • David P. SmithJane M. Lin
    • David P. SmithJane M. Lin
    • F42B1260
    • F42B12/60
    • There is provided a countermeasure defense system against hostile missiles by employing non-explosive intercepting (“NEI”) elements 14 deployed by the spin stabilized rocket 10. The NEI are carried in a payload section 17 and contained by a sleeve assembly 16 which is removed by a drive mechanism 20 or a pyrotechnic device 152 after a countdown time delay programmed into the trigger release assembly 46 as controlled by the control unit 150. The drive assembly includes a drive rod 26 that is releasably held by a release assembly 46 a compressed coiled spring unit 30 drives the sleeve assembly 16 forward exposing the payload section 17 to the centrifugal force of the spin stabilized rocket propelling the NEI elements out from the rocket at constant angular velocity creating an interceptor cloud of elements. In another embodiment the pyrotechnic device 152 detaches the shearable screws 170 that secure the payload section 117 from the rocket engine housing 102 thereby setting the sleeve 121 free from the rocket housing 102.
    • 通过采用由自旋稳定火箭10部署的非易爆拦截(“NEI”)元件14,提供了针对敌对导弹的对策防御系统。该NEI载入有效载荷部分17,并由套筒组件16包含,该组件16被移除 通过驱动机构20或烟火装置152在由控制单元150控制的程序进入触发器释放组件46之后的倒计时延时之后。驱动组件包括驱动杆26,驱动杆26由释放组件46可释放地保持,压缩卷 弹簧单元30驱动套筒组件16向前使有效载荷部分17暴露于旋转稳定的火箭的离心力,其以恒定的角速度将NEI元件从火箭推出,产生元件的拦截云。 在另一个实施例中,烟火装置152分离将有效载荷部分117从火箭发动机壳体102固定的可剪切螺钉170,从而将套筒121设置成不受火箭壳体102的影响。