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    • 5. 发明授权
    • Diamond deposition cell
    • 金刚石沉积池
    • US5182093A
    • 1993-01-26
    • US462496
    • 1990-01-08
    • Gordon L. Cann
    • Gordon L. Cann
    • C23C16/27C23C16/44C30B25/02
    • C23C16/44C23C16/27C30B25/02C30B29/04Y10S427/103
    • In a first embodiment of an improved diamond deposition cell, a chamber is evacuated to a low pressure and a graphite element in the chamber is heated to a selected high temperature and heats a substrate positioned within the chamber spaced by a selected gap from the graphite body to a selected lower temperature. Hydrogen or a mixture of hydrogen and hydrocarbon gas is admitted to the chamber and part of the hydrogen reacts with the hot graphite body to form atomic hydrogen and hydrocarbon gasses. Hydrogen and hydrocarbon gasses cycle repeatedly across the gap between the facing surfaces of the body and the substrate in the kinetic regime resulting in a net transfer of carbon to the substrate and its deposition as diamond crystals or film on the substrate. In a second embodiment, the graphite body is heated by combusting gasses in a cavity therein. Products of such combustion, hydrogen and, optionally, additional hydrocarbon gas are admitted to the gap between the surfaces of the graphite body and the substrate. The temperatures of the facing surfaces, the pressure in the gap and the ratio of the constituent gasses results in carbon atoms being deposited on the substrate in the form of diamond film and other carbon products.
    • 在改进的金刚石沉积池的第一实施例中,将室抽真空至低压,并且将室中的石墨元件加热至选定的高温,并将位于腔室内的基板与石墨体间隔开选定的间隙 到选定的较低温度。 氢气或氢气和烃气体的混合物进入室,部分氢气与热石墨体反应形成原子氢和烃气。 氢气和碳氢化合物在动力学状态下重复地跨越体的相对表面和基底之间的间隙循环,导致碳向衬底的净转移并且其作为金刚石晶体或膜沉积在衬底上。 在第二实施例中,通过在其中的空腔中燃烧气体来加热石墨体。 这种燃烧的产物,氢气和任选的另外的烃气体被允许进入石墨体和衬底的表面之间的间隙。 面向表面的温度,间隙中的压力和构成气体的比例导致碳原子以金刚石膜和其它碳产物的形式沉积在基底上。
    • 6. 再颁专利
    • Heater/emitter assembly
    • 加热器/发射器组件
    • USRE32918E
    • 1989-05-09
    • US930101
    • 1986-11-13
    • Gordon L. Cann
    • Gordon L. Cann
    • B64G1/40F02K9/68
    • F02K9/68B64G1/405B64G1/406
    • A heater/emitter for a rocket engine assembly utilizes a resistance heated wire coil or coils which may also function as a cathode emitter or as a thermal driver for an auxiliary emitter. This heater/emitter may if desired be formed into a bifilar and may be supported by the wire lead itself or by isolated supports. The power leads are located in a lead channel and feature an overwrapping of similar wire material which reduces the internal resistance heating of the lead to increase the electrical conductivity of the supporting lead and increase the thermal conduction thereof to establish a cooler and structurally-stronger lead. A plurality of radiation discs or shields are spaced along the leads to further minimize energy losses from the heater out of the lead channel. The heater/emitter itself is enclosed, except for the lead channel, by a heat exchanger housing. The function of this housing is to accept energy from the hot heater coil and in turn transfer that energy to a fluid flowing through the heat exchanger. Power is transferred from the hot heater coil to the heat exchanger firstly by means of radiation heat transfer, and secondly by impingement of thermionic electrons accelerated thru a potential imposed between the emitter and the heat exchanger. This packaging approach permits radiation transfer efficiencies, from coil to heat exchanger, of 90 to 95 percent. The thermionic electron emission and acceleration efficiency approaches 100 percent. The dual energy transfer mode permits single device operation over wider power ranges and thrust levels than would be permitted by single mode devices. The device may be operated in the single mode as a radiation transfer heater or as a combination radiator and emitter, or may function with the principal energy transfer being in the emitter mode only.
    • 7. 发明授权
    • Micro-arc milling of metallic and non-metallic substrates
    • 金属和非金属基板的微弧铣削
    • US4495399A
    • 1985-01-22
    • US354546
    • 1982-03-04
    • Gordon L. Cann
    • Gordon L. Cann
    • B23K9/23H05K1/00H05K3/00B23K9/00
    • B23K9/23H05K3/0041H05K1/0298H05K2203/081H05K2203/095H05K2203/1105
    • By using a controlled arc-heated gas flow, material may be milled away from a substrate. By controlling the size of a gas flow aperture as well as other variables such as gas flow and arc current, small holes can be drilled into the substrate. Typically, these holes would have a diameter between 0.025 mm and 0.125 mm.In one embodiment, an arc made between an anode and cathode is placed above the work. A gas vortex is produced and is caused to pass through the arc, with the holes being drilled by the heated high-energy gas. Alternatively, the work may be used as the anode, with the gas flow carrying away material heated at the arc attachment point of the anode.The use of the arc-generated plasma gas vortex is particularly advantageous in the milling of multi-layer circuit boards.
    • 通过使用可控制的电弧加热气流,材料可以从衬底上研磨掉。 通过控制气流孔径的尺寸以及气流和电弧电流等其它变量,可以在基板上钻出小孔。 通常,这些孔的直径为0.025mm至0.125mm。 在一个实施例中,在阳极和阴极之间形成的电弧放置在工件上方。 产生气体涡流并使其通过电弧,孔被加热的高能气体钻探。 或者,可以将工件用作阳极,气流携带在阳极的电弧附着点加热的材料。 使用电弧产生的等离子体气体涡流在多层电路板的铣削中是特别有利的。
    • 10. 发明授权
    • Heater/emitter assembly
    • 加热器/发射器组件
    • US4569198A
    • 1986-02-11
    • US735301
    • 1985-05-17
    • Gordon L. Cann
    • Gordon L. Cann
    • B64G1/40F02K9/68H05B3/42H05B1/00
    • B64G1/406B64G1/405F02K9/68H05B3/42
    • A heater/emitter for a rocket engine assembly utilizes a resistance heated wire coil or coils which may also function as a cathode emitter or as a thermal driver for an auxiliary emitter. This heater/emitter may if desired be formed into a bifilar and may be supported by the wire lead itself or by isolated supports. The power leads are located in a lead channel and feature an overwrapping of similar wire material which reduces the internal resistance heating of the lead to increase the electrical conductivity of the supporting lead and increase the thermal conduction thereof to establish a cooler and structurally-stronger lead. A plurality of radiation discs or shields are spaced along the leads to further minimize energy losses from the heater out of the lead channel. The heater/emitter itself is enclosed, except for the lead channel, by a heat exchanger housing. The function of this housing is to accept energy from the hot heater coil and in turn transfer that energy to a fluid flowing through the heat exchanger. Power is transferred from the hot heater coil to the heat exchanger firstly by means of radiation heat transfer, and secondly by impingement of thermionic electrons accelerated thru a potential imposed between the emitter and the heat exchanger. This packaging approach permits radiation transfer efficiencies, from coil to heat exchanger, of 90 to 95 percent. The thermionic electron emission and acceleration efficiency approaches 100 percent. The dual energy transfer mode permits single device operation over wider power ranges and thrust levels than would be permitted by single mode devices. The device may be operated in the single mode as a radiation transfer heater or as a combination radiator and emitter, or may function with the principal energy transfer being in the emitter mode only.
    • 用于火箭发动机组件的加热器/发射器使用电阻加热的线圈或线圈,其也可以用作阴极发射器或用作辅助发射器的热驱动器。 如果需要,该加热器/发射器可以形成双头并且可以由导线本身或隔离的支撑件支撑。 电源引线位于引线通道中,并且具有类似线材的外包装,其减少引线的内部电阻加热,以增加支撑引线的导电性并增加其导热,从而建立较冷和结构强的引线 。 多个辐射盘或屏蔽沿着引线间隔开,以进一步最小化从加热器引出通道的能量损失。 加热器/发射器本身由导热通道除外,由热交换器外壳封闭。 该壳体的功能是接受来自热加热器线圈的能量,并将能量转移到流过热交换器的流体。 电力首先通过辐射热传递从热加热器线圈传递到热交换器,其次是通过在发射器和热交换器之间施加的电势加速的热离子电子的冲击。 这种包装方法允许从线圈到热交换器的辐射传递效率为90%至95%。 热离子电子发射和加速效率接近100%。 双能量传输模式允许单个设备在比单模设备允许的更宽的功率范围和推力水平下工作。 该装置可以以单一模式作为辐射传递加热器或作为辐射器和发射器的组合操作,或者可以仅在主发射器模式下进行主能量传递。