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1. 发明授权

US06641074B2 Seat belt webbing pretensioner using MEMS devices 有权
标题翻译：使用MEMS器件的安全带安全带预紧器
公开(公告)号：US06641074B2
公开(公告)日：2003-11-04
申请号：US09756409
申请日：2001-01-08
申请人： Christopher C. Shih , Douglas P. Campbell , Lee D. Bergerson , Dean M. Esterberg , Paul A. Bowers , Ernst M. Faigle , Homer W. Fogle, Jr. , Ivan L. Stonich , David H. Lewis, Jr. , Eric N. Streif , Brian R. Pitstick , Timothy A. Swann , Roy D. Van Wynsberghe
发明人： Christopher C. Shih , Douglas P. Campbell , Lee D. Bergerson , Dean M. Esterberg , Paul A. Bowers , Ernst M. Faigle , Homer W. Fogle, Jr. , Ivan L. Stonich , David H. Lewis, Jr. , Eric N. Streif , Brian R. Pitstick , Timothy A. Swann , Roy D. Van Wynsberghe
IPC分类号： B60R2246
CPC分类号： B60R22/4633 , B60R2021/26029 , B60R2022/4657 , B60R2022/4685 , C06D5/00
摘要： A pretensioner (50) tensions vehicle seat belt webbing (18). The pretensioner (50) has a member (52) movable by an actuating fluid to tension the seat belt webbing (18). The pretensioner (50) further has at least one microelectromechanical system (MEMS) device (120) energizable to supply actuating fluid to move the member (52).
摘要翻译：预紧器（50）张紧车辆安全带安全带（18）。预紧器（50）具有可由致动流体移动的构件（52），以张紧座椅安全带织带（18）。预张紧器（50）还具有至少一个微机电系统（MEMS）装置（120），该微机电系统（120）可通电以供应致动流体以移动构件（52）。

2. 发明授权

US6131385A Integrated pulsed propulsion system for microsatellite 失效
标题翻译：用于微卫星的集成脉冲推进系统
公开(公告)号：US6131385A
公开(公告)日：2000-10-17
申请号：US912709
申请日：1997-08-18
申请人： David H. Lewis, Jr. , Erik K. Antonsson
发明人： David H. Lewis, Jr. , Erik K. Antonsson
IPC分类号： B64G1/00 , F02K9/94 , F02K99/00 , F03H99/00 , F15B15/14 , F03H5/00
CPC分类号： F02K9/94 , F15B15/1471
摘要： A propulsion system and, in particular, a microthruster for a microsatellite. The microthruster may be formed as a resistojet type thruster formed with a chamber, closed by a diaphragm which acts as a blow-out disk. A fluid, such as an inert gas, is disposed within the chamber. Heating of the gas causes the gas pressure to increase until the diaphragm ruptures, which, in turn, causes the gas to flow out of the chamber, acting as a propellant, and providing a small unit force. The microthruster is adapted to be formed by known batch processing methods with 10.sup.4 -10.sup.6 microthrusters per wafer. The unit of force can be easily scaled by varying the number of microthruster 20 used for an application, the geometry of the chamber 22, as well as the type of fluid used within the chamber, to suit the microsatellite application.
摘要翻译：推进系统，特别是用于微卫星的微型推进器。微型推进器可以形成为形成有腔室的再喷射式推进器，该室由作为吹出盘的隔膜封闭。诸如惰性气体的流体设置在室内。气体的加热导致气体压力增加，直到膜片破裂，这又导致气体流出室，用作推进剂，并提供小的单位力。微型推杆适用于通过已知的批量处理方法形成，每个晶片具有104-106个微型推进器。可以通过改变用于应用的微推力器20的数量，室22的几何形状以及室内使用的流体的类型来适应微卫星应用来容易地缩放力单位。

3. 发明授权

US06861170B2 Volumetric micro batteries 有权
标题翻译：体积微电池
公开(公告)号：US06861170B2
公开(公告)日：2005-03-01
申请号：US09948034
申请日：2001-09-05
申请人： David H. Lewis, Jr. , John J. Waypa , Erik K. Antonsson , Charles D. E. Lakeman
发明人： David H. Lewis, Jr. , John J. Waypa , Erik K. Antonsson , Charles D. E. Lakeman
IPC分类号： H01M4/24 , H01M4/86 , H01M4/96 , H01M10/04 , H01M12/06 , H01M6/04
CPC分类号： H01M4/244 , H01M4/8605 , H01M4/96 , H01M10/0472 , H01M12/06
摘要： A microelectronic battery is formed from Zn/Air technology as a volumetric energy storage device from soft lithography techniques. The microelectric battery includes an anode and a cathode disposed in an electrolyte tank having a volume
摘要翻译：微电子电池由Zn / Air技术形成为软光刻技术的体积储能装置。微电池包括设置在电解槽中的阳极和阴极，该电解槽具有填充有电解质的体积<1MM 3。

4. 发明授权

US06621687B2 Micro-supercapacitor 有权
标题翻译：微型超级电容器
公开(公告)号：US06621687B2
公开(公告)日：2003-09-16
申请号：US09948033
申请日：2001-09-05
申请人： David H. Lewis, Jr. , John J. Waypa , Erik K. Antonsson , Charles D. E. Lakeman
发明人： David H. Lewis, Jr. , John J. Waypa , Erik K. Antonsson , Charles D. E. Lakeman
IPC分类号： H01G904
CPC分类号： H01G9/155 , H01M6/181 , H01M6/40 , H01M10/0436 , Y02E60/13
摘要： A microelectronic supercapacitor is amenable to being fabricated using micro electromechanical systems (MEMS) techniques. By utilizing MEMS techniques, the supercapacitor in accordance with the present invention can be formed with volumes
摘要翻译：微电子超级电容器适于使用微机电系统（MEMS）技术制造。通过利用MEMS技术，根据本发明的超级电容器可以以<1mm 3的体积形成。因此，这种微电子超级电容器适用于只有几毫米可用于超级电容器和诸如电池的能量存储装置的应用中。

5. 发明授权

US06431071B1 Mems arm fire and safe and arm devices 失效
标题翻译：手臂防火，安全和手臂装置
公开(公告)号：US06431071B1
公开(公告)日：2002-08-13
申请号：US09665230
申请日：2000-09-18
申请人： Kathleen F. Hodge , David H. Lewis, Jr. , Steven D. Nelson , Victor W. Ruwe
发明人： Kathleen F. Hodge , David H. Lewis, Jr. , Steven D. Nelson , Victor W. Ruwe
IPC分类号： F42C1526
CPC分类号： F42C15/36 , F42C15/184 , F42C15/34 , F42C15/40
摘要： Miniature arm fire and safe and arm devices include an electrically operated pyrotechnic initiation device (5) to generate a detonation wave upon command and a movable pressure barrier (9) that blocks propagation of the detonation wave if the device is not intended to be fired and opens a window (12) to transfer the detonation wave externally of the device. The detonation wave may in alternate embodiments be a subsonic flame front and pressure wave or a supersonic shock wave, respectively. An electromagnet (7) may serve to move the pressure barrier. Detonation waves output from the device have application in igniting an explosive train, either directly or indirectly, the latter by operating an electrical switch. In the arm fire device, the barrier automatically prevents a detonation output when electrical power is removed from the device. In the safe and arm device, the barrier, once moved out of the way, remains out of the way, even when electrical power is removed. Various forms of miniature single operate electrical switches are described that may be operated by the foregoing devices.
摘要翻译：微型手臂式防火和安全和手臂装置包括电动式烟火引发装置（5），用于在命令时产生爆震波;以及可移动压力屏障（9），其阻止爆震波的传播，如果该装置不打算被点燃，打开窗口（12）以将设备外部的爆震波转移。在替代实施例中，爆震波分别是亚音速火焰前和压力波或超音速冲击波。电磁体（7）可用于移动压力屏障。从设备输出的爆震波可以通过操作电气开关直接或间接点燃爆炸火车。在手臂消防装置中，当从设备中取出电力时，屏障自动防止爆震输出。在安全和手臂装置中，障碍物一旦被移开，即使在电力消除的情况下仍然存在。描述了可由前述装置操作的各种形式的微型单操作电开关。

6. 发明授权

US06216445B1 Micro pulsed plasma thruster and method of operating same 失效
标题翻译：微脉冲等离子体推进器及其运行方法
公开(公告)号：US06216445B1
公开(公告)日：2001-04-17
申请号：US09315211
申请日：1999-05-19
申请人： David C. Byers , David H. Lewis, Jr.
发明人： David C. Byers , David H. Lewis, Jr.
IPC分类号： G21D100
CPC分类号： F03H1/0087 , F03H1/0012
摘要： A pulse plasma thruster (50) utilizes a vapor producing solid (54) and a micro-sized heater (52) to produce a high pressure vapor that is directed into an ignition chamber (58) and to a thrust discharge chamber (70). The thrust discharge chamber (70) comprises two oppositely disposed electrode plates (72, 74) and oppositely disposed fuel propellants sources (60, 62). The passageway (56) leading from vapor producing solid (54) to the thrust discharge chamber (70) is configured to permit uniform feeding of the vapors to the thrust discharge chamber (70). A pair of electrode terminals (82, 84) extend from the electrode plates (72, 74) and through a housing (88). A power source (100) is coupled to the terminals (82, 84) and provides the ignition signals necessary to cause a spark and a breakdown to a useful plasma arc by controlling the voltage-current shape of the ignition signal.
摘要翻译：脉冲等离子体推进器（50）利用蒸汽产生固体（54）和微型加热器（52）来产生被引导到点火室（58）和推力释放室（70）中的高压蒸汽。推力排放室（70）包括两个相对设置的电极板（72,74）和相对设置的燃料推进剂源（60,62）。从产生气体的固体（54）引导到推力排出室（70）的通道（56）被构造成允许蒸汽均匀地进给推力排出室（70）。一对电极端子（82,84）从电极板（72,74）延伸并穿过壳体（88）。电源（100）耦合到端子（82,84），并且通过控制点火信号的电压 - 电流形状来提供引起火花和击穿有用等离子体电弧所必需的点火信号。

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