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    • 1. 发明授权
    • Spacecraft payload exchange system
    • 航天器有效载荷交换系统
    • US5429328A
    • 1995-07-04
    • US977075
    • 1992-11-16
    • Michael E. DobbsDonald B. Jones
    • Michael E. DobbsDonald B. Jones
    • B64G1/64
    • B64G1/646B64G1/641
    • A method of manufacturing in space and a spacecraft assembly to accomplish such manufacture. The spacecraft assembly includes a spacecraft including a plurality of canister compartments circumferentially spaced about the central axis of the spacecraft and opening in a docking face of the spacecraft, a plurality of canisters respectively positioned in the compartments, and a passive docking mechanism proximate the docking face and proximate the central axis, and a service vehicle comprising a plurality of canister compartments spaced circumferentially about the central axis of the service vehicle, a plurality of canisters respectively positioned in the compartments, and a manipulator assembly including an active docking structure, including a boom extending forwardly from the docking face, and a canister handling assembly mounted on the boom. In one embodiment, the spacecraft remains permanently in orbit, a manufacturing process is performed on the spacecraft to produce an end product which is housed in the canisters, and the service vehicle periodically visits the orbiting spacecraft to perform a canister exchange with the spacecraft, utilizing the canister exchange with the spacecraft, utilizing the canister handling assembly, and replenishing the spacecraft supplies.
    • 空间制造方法和航天器组件来实现这种制造。 航天器组件包括航天器,其包括围绕航天器的中心轴线周向隔开并在飞船的对接面上开口的多个罐隔室,分别定位在舱室中的多个罐和靠近对接面的被动对接机构 并且靠近中心轴线,以及服务车辆,其包括围绕服务车辆的中心轴线周向间隔开的多个罐室,分别定位在隔间中的多个罐,以及包括主动对接结构的操纵器组件,包括吊杆 从对接面向前延伸,以及安装在起重臂上的罐处理组件。 在一个实施例中,航天器永久地保持在轨道上,对航天器执行制造过程以产生容纳在罐中的最终产品,并且服务车辆周期性地访问轨道航天器以与飞船进行罐交换,利用 罐与飞船交换,利用罐处理组件,并补充航天器耗材。
    • 2. 发明授权
    • Automatic compliant capture and docking mechanism for spacecraft
    • 用于航天器的自动兼容捕获和对接机制
    • US5364046A
    • 1994-11-15
    • US839996
    • 1992-02-24
    • Michael E. DobbsPeter Tchoryk, Jr.Donald B. Jones
    • Michael E. DobbsPeter Tchoryk, Jr.Donald B. Jones
    • B64G1/64B64G1/62
    • B64G1/646Y10T292/14
    • This invention is an automatic capture and docking mechanism for a pair of spacecraft. A largely passive capture mechanism disposed on a first spacecraft includes a concave cone section with the narrower interior end to admit a ball of a predetermined diameter. When tripped, a capture device restricts the diameter of passage for capture of the ball. In the release position passage for the ball is unrestricted. The capture device is preferably reset by the other spacecraft to release the ball. A docking mechanism disposed on the second spacecraft includes a convex cone section constructed to mate with the concave cone section, ball at the end of a cable and a boom. The cable may be extended from or retracted to the apex of the convex cone section. A rotary drive coupled to the convex cone section permits relative rotation of the spacecraft. The boom may be extended from or retracted into the second spacecraft. The spacecraft dock by directing the extended ball into the cylinder, where it is captured. The cable and boom retract to dock. The active docking mechanism releases and resets the capture device to undock. A pyrotechnic cutter disposed inside the boom can cut the cable for emergency release.
    • 本发明是用于一对航天器的自动捕获和对接机构。 设置在第一航天器上的主要被动捕获机构包括具有较窄内部端部以容纳预定直径的球的凹形锥形部分。 当跳闸时,捕获装置限制通道的直径以捕获球。 在球的释放位置通道是不受限制的。 捕获装置优选由另一个航天器复位以释放球。 设置在第二航天器上的对接机构包括构造成与凹锥部分配合的凸锥部分,电缆端部处的球和吊杆。 电缆可以从凸锥部分的顶点延伸或缩回到凸锥部分的顶点。 联接到凸锥部的旋转驱动器允许航天器的相对旋转。 悬臂可以从第二个航天器延伸或缩回到第二个航天器。 通过将延伸的球引导到气缸中,在那里被捕获,该航天器基座。 电缆和吊杆缩回到码头。 主动对接机制释放并重置捕获设备以停用。 布置在吊臂内部的烟火切割机可以切断电缆以便紧急释放。
    • 3. 发明授权
    • Robotic substrate manipulator
    • 机器人基板操纵器
    • US5271702A
    • 1993-12-21
    • US829719
    • 1992-02-03
    • Michael E. DobbsDonald B. Jones
    • Michael E. DobbsDonald B. Jones
    • B65G49/07H01L21/687
    • H01L21/68707Y10S414/137Y10S414/139Y10S414/141
    • A robotic substrate manipulator constructed for substrate handling during thin film deposition in the vacuum of outer space. The robotic substrate manipulator includes a cassette holding a plurality of substrates preferably including six cassettes in a carousel. A circular cylinder encloses the carousel with an access door at a location accessible by a manipulator arm assembly. Substrates are retained within the cassette via a passive retention system. This manipulator arm assembly includes an arm with a gripper at one end. The gripper includes a pair of opposed fingers normally urged closed by at least one finger spring that may be opened by a solenoid. The manipulator arm assembly includes a vertical driver and a horizontal rotary driver permitting motion of substrates from the cassette to a processing station. Position gauges on both the vertical motion driver and the horizontal rotary motion driver permit feedback regarding the manipulator arm assembly position. In the preferred embodiment the processing station employs the vacuum of space in thin film deposition.
    • 一种机器人基板操纵器,其构造用于在外层空间的真空中薄膜沉积期间的基板处理。 机器人衬底操纵器包括容纳多个衬底的盒,其优选地包括在转盘中的六个盒。 圆形圆柱体在转盘附近具有通道门,可由操纵臂组件接近。 基板通过被动保持系统保持在盒内。 该操纵臂组件包括在一端具有夹持器的臂。 夹具包括一对相对的手指,通常由可由螺线管打开的至少一个手指弹簧关闭。 操纵臂组件包括垂直驱动器和水平旋转驱动器,其允许基板从盒带运动到处理站。 垂直运动驱动器和水平旋转运动驱动器上的位置测量器允许关于操纵臂组件位置的反馈。 在优选实施例中,处理站采用薄膜沉积中的空间真空。
    • 6. 发明授权
    • Active remote sensing using lock-in amplifiers and beam steering
    • 使用锁定放大器和波束转向的主动遥感
    • US07009705B1
    • 2006-03-07
    • US10197247
    • 2002-07-18
    • Michael E. DobbsAllan Roberts
    • Michael E. DobbsAllan Roberts
    • G01N21/55
    • G01S17/87G01S7/497G01S17/32G01S17/89
    • A remote sensing platform for sensing a target may include a source configured to emit optical radiation toward the target. A device may be configured to dither the emitted optical radiation to alternately illuminate a number of locations on the target. A first detector may be configured to detect radiation reflected from a first location of the number of locations and to generate a first signal. A first lock-in amplifier may be configured to process the first signal. A second detector may be configured to detect radiation reflected from a second location of the number of locations and to generate a second signal. A second lock-in amplifier may be configured to process the second signal.
    • 用于感测目标的遥感平台可以包括被配置为朝向目标发射光辐射的源。 设备可以被配置为使所发射的光辐射抖动以交替地照射目标上的多个位置。 第一检测器可以被配置为检测从位置的数量的第一位置反射的辐射并且产生第一信号。 第一锁定放大器可以被配置为处理第一信号。 第二检测器可以被配置为检测从位置的数量的第二位置反射的辐射并且产生第二信号。 第二锁定放大器可以被配置为处理第二信号。