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    • 1. 发明授权
    • Unitary fingerboard and method of making same
    • 单一指板及其制作方法
    • US07763786B2
    • 2010-07-27
    • US12105836
    • 2008-04-18
    • Donald B. JonesDouglas D. Jones
    • Donald B. JonesDouglas D. Jones
    • G10D3/06
    • G10D3/06
    • A stringed musical instrument has a head assembly, a tail, and an elongate neck extending from the head assembly to the tail. The neck defines a fingerboard having a surface layer and a substrate. The surface layer includes an exposed surface formed of sheet metal deformed to unitarily define a plurality of frets thereon. A plurality of strings extends from the head assembly along the neck and adjacent to the fingerboard. In another variation, the surface layer has an exposed surface unitarily defining frets thereon. Each fret forms a peak, and the surface layer defines a plurality of troughs separated by the peaks. Each trough has a single arcuate shape extending between each peak. A method of forming the stringed musical instrument is also disclosed.
    • 弦乐器具有头部组件,尾部和从头部组件延伸到尾部的细长颈部。 颈部限定具有表面层和基底的指板。 表面层包括由金属板形成的暴露表面,其被变形以在其上整体地限定多个电荷。 多个弦从头部组件沿颈部延伸并且邻近指板。 在另一个实施方式中,表面层具有在其上一体地限定光泽的暴露表面。 每个毛毡形成一个峰,并且表面层限定了由峰分开的多个槽。 每个槽具有在每个峰之间延伸的单个弓形形状。 还公开了一种形成弦乐器的方法。
    • 2. 发明申请
    • UNITARY FINGERBOARD AND METHOD OF MAKING SAME
    • 单位指纹板及其制作方法
    • US20080190264A1
    • 2008-08-14
    • US12105836
    • 2008-04-18
    • Donald B. JonesDouglas D. Jones
    • Donald B. JonesDouglas D. Jones
    • G10D3/06
    • G10D3/06
    • A stringed musical instrument has a head assembly, a tail, and an elongate neck extending from the head assembly to the tail. The neck defines a fingerboard having a surface layer and a substrate. The surface layer includes an exposed surface formed of sheet metal deformed to unitarily define a plurality of frets thereon. A plurality of strings extends from the head assembly along the neck and adjacent to the fingerboard. In another variation, the surface layer has an exposed surface unitarily defining frets thereon. Each fret forms a peak, and the surface layer defines a plurality of troughs separated by the peaks. Each trough has a single arcuate shape extending between each peak. A method of forming the stringed musical instrument is also disclosed.
    • 弦乐器具有头部组件,尾部和从头部组件延伸到尾部的细长颈部。 颈部限定具有表面层和基底的指板。 表面层包括由金属板形成的暴露表面,其被变形以在其上整体地限定多个电荷。 多个弦从头部组件沿颈部延伸并且邻近指板。 在另一个实施方式中,表面层具有在其上一体地限定光泽的暴露表面。 每个毛毡形成一个峰,并且表面层限定了由峰分开的多个槽。 每个槽具有在每个峰之间延伸的单个弓形形状。 还公开了一种形成弦乐器的方法。
    • 3. 发明授权
    • Electrostatic deposition of charged coating particles onto a dielectric
substrate
    • 带电涂层颗粒静电沉积到电介质基片上
    • US5830274A
    • 1998-11-03
    • US575188
    • 1995-12-20
    • Donald B. JonesLeland H. CarlblomKen W. NiederstPaul S. Chirgott
    • Donald B. JonesLeland H. CarlblomKen W. NiederstPaul S. Chirgott
    • B05B5/043B05B5/08B05B5/00
    • B05B5/087B05B5/043B05B5/082Y10S118/03
    • The present invention provides an apparatus for controlling the spray of positively-charged coating particles towards a grounded or negatively-charged dielectric material having a dielectric constant less than 4.0 and in the form of a hollow container. This apparatus includes: (a) a device for inducing a positive charge onto a coating composition, (b) a device for creating a field of positively-charged coating particles, (c) a device for supporting a series of hollow containers in spaced relation to one another which includes a series of vertically-oriented spindles, (d) a device for transporting the spindles in series through the field of positively-charged coating particles, (e) a gripping chuck made from, or coated with, a dielectric material, or both, mounted to the upper end of a spindle, the chuck having a recess defined therein for receiving the opening of a hollow container, and (f) a grounding device positioned such that, when the dielectric container is in the path of the sprayed, positively-charged coating particles the grounding device is also in the path but shielded therefrom by the dielectric material. The grounding device is insulated from direct electrical contact with the supported container. The grounding device can be replaced by an internal charging device for inducing a negative charge onto a hollow container being supported by the gripping chuck. Moreover, the grounding device or the internal charging device can be used in conjunction with an external charging device for inducing a negative charge onto a hollow container being supported by the gripping chuck.
    • 本发明提供了一种用于控制带正电荷的涂层颗粒朝着介电常数小于4.0的接地或带负电荷的电介质材料喷射并且以中空容器的形式的装置。 该装置包括:(a)用于在涂料组合物上引起正电荷的装置,(b)用于产生带正电的涂层颗粒的场的装置,(c)用于以间隔关系支撑一系列中空容器的装置 (d)用于通过带正电荷的涂层颗粒领域串联输送主轴的装置,(e)由介电材料制成或涂覆的夹紧卡盘 或两者安装到主轴的上端,卡盘具有限定在其中的凹部,用于容纳中空容器的开口,以及(f)接地装置,其定位成使得当电介质容器处于 喷涂的带正电荷的涂层颗粒,接地装置也在路径中,但是被电介质材料遮挡。 接地装置与受支撑的容器直接电接触绝缘。 接地装置可以由内部充电装置代替,用于在由卡盘支撑的中空容器上引起负电荷。 此外,接地装置或内部充电装置可以与外部充电装置一起使用,用于将负电荷引导到由夹紧卡盘支撑的中空容器上。
    • 6. 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。
    • 7. 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。
    • 9. 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。