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21. 发明授权

US5927653A Two-stage reusable earth-to-orbit aerospace vehicle and transport system 失效
标题翻译：两级可重用地球对轨道航空航天车辆和运输系统
公开(公告)号：US5927653A
公开(公告)日：1999-07-27
申请号：US632786
申请日：1996-04-17
申请人： George E. Mueller , Walter P. Kistler , Thomas G. Johnson , Henry O. Pohl , Chris McLain , Allan S. Hill , Jason E. Andrews , Thomas C. Taylor , Aaron Cohen , Dale Myers , Adam P. Bruckner , Steven C. Knowles , Richard Warwick
发明人： George E. Mueller , Walter P. Kistler , Thomas G. Johnson , Henry O. Pohl , Chris McLain , Allan S. Hill , Jason E. Andrews , Thomas C. Taylor , Aaron Cohen , Dale Myers , Adam P. Bruckner , Steven C. Knowles , Richard Warwick
IPC分类号： B64G1/00 , B64G1/14 , B64G1/40 , B64G1/62 , B64G1/64 , B64G5/00
CPC分类号： B64G1/401 , B64G1/14 , B64G1/402 , B64G1/62 , B64G1/641 , B64G5/00
摘要： A two-stage wingless reusable aerospace vehicle having upper and lower stages that take off from a take-off area and separate at a separation point along a first trajectory. The separation forces are generated by air retained between the upper and lower stages, which is at a pressure higher than ambient pressure at the separation point. The lower stage is then propelled along a return trajectory to a landing area. After separation from the lower stage, the upper stage continues to an Earth orbit for deployment of a payload. After deploying the payload, the upper stage moves out of the Earth orbit, re-enters the Earth's atmosphere, and returns to the take-off and landing area. The upper and lower stages are powered by liquid oxygen and kerosene engines. The aerospace vehicle is transported to a take-off area by a transport vehicle having a first fixed carriage and a second translatable carriage that is adapted to move the upper stage relative to the lower stage for assembly of the aerospace vehicle while in the horizontal position. The transport vehicle then pivots the aerospace vehicle from the horizontal to the vertical position for launching.
摘要翻译：一种两级无翼可重复使用的航空航天器，具有从起飞区域起飞并且沿着第一轨迹在分离点分离的上段和下段。分离力由保持在上部和下部之间的空气产生，其处于高于分离点处的环境压力的压力。然后，下阶段沿着返回轨迹被推进到着陆区域。在与下级分离之后，上级继续到地球轨道，用于部署有效载荷。部署有效载荷后，上级移出地球轨道，重新进入地球大气层，返回起飞和着陆区域。上层和下层由液氧和煤油发动机提供动力。航空航天车辆通过具有第一固定支架和第二可平移滑架的运输车辆被运送到起飞区域，该第二可平移滑架适于在水平位置组装航空航天器时相对于下部台阶移动。然后，运输车辆将航空航天器从水平轴枢转到用于发射的垂直位置。

22. 发明授权

US4867395A Flat end cap module for space transportation systems 失效
标题翻译：用于空间运输系统的平端盖模块
公开(公告)号：US4867395A
公开(公告)日：1989-09-19
申请号：US858739
申请日：1986-05-01
申请人： Thomas C. Taylor , Robert A. Citron
发明人： Thomas C. Taylor , Robert A. Citron
IPC分类号： B64G1/12 , B64G1/14
CPC分类号： B64G1/14 , B64G1/12
摘要： A module incorporating at least one flat end cap is positioned within the payload of the Space Shuttle or other space vehicle to enhance the capabilities of the payload area. The flat end cap reduces the required volume in the launch vehicle to be occupied by the module and provides for efficient use of the interior space of the Space Shuttle by providing more flat surfaces to which necessary equipment can be fastened. The module is truncated, thus adding another flat surface, i.e., a ceiling, to the interior of the vehicle. The truncated top of the module is capable of separate integration and carries additional experiments within racks which can be attached to its interior surface. The module can be fabricated from aluminum members in an aircraft type fashion of construction, or can be assembled from existing or modified Space Lab hardware. The module provides a full scope of services within its pressurized interior and will enhance the carrying capability of the shuttle with respect to handling both personnel and cargo.

23. 发明授权

US07559509B1 Large cryogenic tank logistics for in-space vehicles 失效
标题翻译：空间车辆的大型低温坦克物流
公开(公告)号：US07559509B1
公开(公告)日：2009-07-14
申请号：US11767459
申请日：2007-06-22
申请人： Walter P. Kistler , Thomas C. Taylor , Robert A. Citron
发明人： Walter P. Kistler , Thomas C. Taylor , Robert A. Citron
IPC分类号： B64G1/00 , B64G1/64
CPC分类号： B64G1/002 , B64G1/007 , B64G1/443 , B64G1/446 , B64G1/62 , B64G1/641 , B64G1/645 , B64G1/646
摘要： An aerospace frame accommodates propellant tanks for facilitating propellant operations in space. The frame includes at least two plates for supporting the propellant tanks; at least one brace supporting the plates; and a cavity between two plates that accommodates a removable propellant tank.
摘要翻译：航空航天框架可容纳推进剂罐，用于促进太空中的推进剂操作。框架包括用于支撑推进剂罐的至少两个板; 支撑板的至少一个支架; 以及容纳可拆卸推进剂罐的两个板之间的空腔。

24. 发明授权

US07559508B1 Propellant depot in space 失效
标题翻译：推进剂仓库在太空
公开(公告)号：US07559508B1
公开(公告)日：2009-07-14
申请号：US11608221
申请日：2006-12-07
申请人： Thomas C. Taylor , Walter P. Kistler , Robert A. Citron
发明人： Thomas C. Taylor , Walter P. Kistler , Robert A. Citron
IPC分类号： B64G1/00
CPC分类号： B64G1/242 , B64G1/002 , B64G1/12 , B64G1/14 , B64G1/16 , B64G1/24 , B64G1/402 , B64G1/403 , B64G1/44 , B64G1/62 , B64G1/646 , B64G1/648 , B64G2001/1064 , B64G2001/1071
摘要： A space transportation propellant depot has multiple locations, sources and capabilities. Maximizing known mature technologies coupled with realistic industrial techniques results in the incremental development of a propellant source on the moon. Propellant depots are economically driven locations with defined services, sources of propellant and innovation in the pursuit of transportation related commerce as mankind explores for resources beyond Earth.
摘要翻译：太空运输推进剂库具有多个位置，来源和能力。最大化已知的成熟技术加上现实的工业技术导致月球上推进剂来源的增量发展。推进剂仓库是经济驱动的地点，具有定义的服务，推动剂的来源和追求运输相关商业的创新，人类探索地球以外的资源。

25. 发明申请

US20090050745A1 COMMERCIAL EXTERNAL RE-ENTRY TESTING FROM ORBIT 审中-公开
标题翻译：从ORBIT进行的商业外部重新进入测试
公开(公告)号：US20090050745A1
公开(公告)日：2009-02-26
申请号：US12041566
申请日：2008-03-03
申请人： George E. Mueller , Gary Lai , Thomas C. Taylor
发明人： George E. Mueller , Gary Lai , Thomas C. Taylor
IPC分类号： B64G1/00
CPC分类号： B64G1/62 , B64G1/105 , B64G1/14 , B64G1/58 , B64G1/641
摘要： An experiment system with six different re-entry experiment locations for testing high temperature re-entry materials, creating new thermal protection systems, proving innovative new concepts for spacecraft exterior surfaces and the incremental development of next generation aerospace materials. A commercial transportation system to and from orbit provides a 24-hour return cycle for the experiments on a surface actually re-entering the earth's atmosphere. Previously expensive arc jet wind tunnels attempted to simulate the re-entry temperatures and ever changing re-entry flow environment for researchers. Now using existing doors, hatches and other points on the reusable launch vehicle's exterior, the actual re-entry environment is experienced by test specimens with quick turn around for a wide variety of different re-entry temperatures ranges for broad testing and development purposes. The reusable launch vehicle launches, remains in orbit for 24 hours and returns to provide an actual test environment for the exterior experiment system.
摘要翻译：具有六个不同重新进入实验位置的实验系统，用于测试高温重入物料，创建新的热保护系统，为航天器外表面提供创新的新概念，以及下一代航空材料的增量开发。往返轨道的商业运输系统为实际重新进入地球大气层的表面提供了24小时的循环。以前昂贵的电弧喷流风洞试图模拟再入境温度和不断变化的研究人员的再入流环境。现在在可重复使用的运载火箭的外部使用现有的门，舱口和其他点，实际的重入环境经历了快速转弯的各种不同的重新进入温度范围，用于广泛的测试和开发目的。可重复使用的运载火箭发射，保持在轨道上24小时，并返回，为外部实验系统提供实际的测试环境。

26. 发明授权

US07229543B2 Apparatus for controlling and/or measuring additive concentration in an electroplating bath 有权
标题翻译：用于控制和/或测量电镀浴中的添加剂浓度的装置
公开(公告)号：US07229543B2
公开(公告)日：2007-06-12
申请号：US10372955
申请日：2003-02-26
申请人： Lyndon W. Graham , Thomas C. Taylor , Thomas L. Ritzdorf , Fredrick A. Lindberg , Bradley C. Carpenter
发明人： Lyndon W. Graham , Thomas C. Taylor , Thomas L. Ritzdorf , Fredrick A. Lindberg , Bradley C. Carpenter
IPC分类号： C25D21/12 , G01F1/64 , G01N27/26 , G01N27/42
CPC分类号： G01N27/48 , G01N27/4161
摘要： A method for measuring a target constituent of an electroplating solution using an electroanalytical technique is set forth in which the electroplating solution includes one or more constituents whose by-products skew an initial electrical response to an energy input of the electroanalytical technique. The method comprises a first step in which an electroanalytical measurement cycle of the target constituent is initiated by providing an energy input to a pair of electrodes disposed in the electroplating solution. The energy input to the pair of electrodes is provided for at least a predetermined time period corresponding to a time period in which the electroanalytical measurement cycle reaches a steady-state condition. In a subsequent step, an electroanalytical measurement of the energy output of the electroanalytical technique is taken after the electroanalytical measurement cycle has reached the steady-state condition. The electroanalytical measurement is then used to determine an amount of the target constituent in the electroplating solution. An automatic dosing system that includes the foregoing method and/or one or more known electroanalytical techniques in a close-loop system is also set forth.
摘要翻译：提出了一种使用电分析技术测量电镀溶液的目标成分的方法，其中电镀溶液包括一种或多种成分，其中副产物偏置对电分析技术的能量输入的初始电响应。该方法包括第一步骤，其中通过向布置在电镀溶液中的一对电极提供能量输入来启动目标成分的电分析测量循环。输入到该对电极的能量被提供至少一个对应于电分析测量周期达到稳态条件的时间段的预定时间段。在随后的步骤中，在电分析测量循环达到稳态条件之后，进行电分析技术的能量输出的电分析测量。然后使用电分析测量来确定电镀溶液中的目标成分的量。还提出了一种包括前述方法和/或闭环系统中的一种或多种已知电分析技术的自动计量系统。

27. 发明授权

US07163179B1 Commercial service platform in space 失效
标题翻译：空间商业服务平台
公开(公告)号：US07163179B1
公开(公告)日：2007-01-16
申请号：US10987088
申请日：2004-11-12
申请人： Thomas C. Taylor
发明人： Thomas C. Taylor
IPC分类号： B64G1/10
CPC分类号： B64G1/1078 , B64G4/00 , B64G2001/224 , G09F15/0025 , G09F21/06
摘要： Affordable commercial service platforms in space focusing on customer affordability, quality microgravity services, innovation and combining five emerging space technologies. The invention provides an integrated approach to microgravity services in orbit. First, the reusable launch vehicle (RLV) offers affordable transportation services, platform reboost, and eliminates platform subsystems of propulsion, RCS, liquid storage/resupply, and the like. Second, deployable structures are not heavy for the launch, but expand in orbit. Third, orbital phone networks offer customers control of unmanned experiments. Fourth, an enhanced robotic system transfers payloads. Fifth, manufactured thin film solar cells in orbit offer advantages including weight/cost reductions. The orbital service platform has a low initial cost, expands as the market demands, is repairable, offers quality unmanned microgravity, leads to production facilities using similar hardware and offers numerous affordable commercial services.
摘要翻译：负担得起的空间商业服务平台专注于客户的负担能力，优质的微重力服务，创新和结合五种新兴的空间技术。本发明提供了在轨道上的微重力服务的综合方法。首先，可重复使用的运载火箭（RLV）提供经济实惠的运输服务，平台重新启动，消除推进，RCS，液体储存/补给等平台子系统。第二，可部署的结构对于发射并不重要，但在轨道上扩展。第三，轨道电话网络为客户提供无人实验的控制。第四，增强的机器人系统传输有效载荷。第五，在轨道上制造的薄膜太阳能电池提供了重量/成本降低的优点。轨道服务平台具有较低的初始成本，随着市场需求的扩大，可修复，提供优质的无人微重力，引导使用类似硬件的生产设施，并提供众多价格实惠的商业服务。

28. 再颁专利

USRE38931E1 Methods for controlling and/or measuring additive concentration in an electroplating bath 有权
标题翻译：用于控制和/或测量电镀浴中的添加剂浓度的方法
公开(公告)号：USRE38931E1
公开(公告)日：2006-01-10
申请号：US10266966
申请日：2003-02-27
申请人： Lyndon W. Graham , Thomas C. Taylor , Thomas L. Ritzdorf , Fredrick A. Lindberg , Bradley C. Carpenter
发明人： Lyndon W. Graham , Thomas C. Taylor , Thomas L. Ritzdorf , Fredrick A. Lindberg , Bradley C. Carpenter
IPC分类号： G01N27/48
CPC分类号： G01N27/4161 , G01N27/48
摘要： A method for measuring a target constituent of an electroplating solution using an electroanalytical technique is set forth in which the electroplating solution includes one or more constituents whose by-products skew an initial electrical response to an energy input of the electroanalytical technique. The method comprises a first step in which an electroanalytical measurement cycle of the target constituent is initiated by providing an energy input to a pair of electrodes disposed in the electroplating solution. The energy input to the pair of electrodes is provided for at least a predetermined time period corresponding to a time period in which the electroanalytical measurement cycle reaches a steady-state condition. In a subsequent step, an electroanalytical measurement of the energy output of the electroanalytical technique is taken after the electroanalytical measurement cycle has reached the steady-state condition. The electroanalytical measurement is then used to determine an amount of the target constituent in the electroplating solution. An automatic dosing system that includes the foregoing method and/or one or more known electroanalytical techniques in a close closed-loop system is also set forth.
摘要翻译：提出了一种使用电分析技术测量电镀溶液的目标成分的方法，其中电镀溶液包括一种或多种成分，其中副产物偏置对电分析技术的能量输入的初始电响应。该方法包括第一步骤，其中通过向布置在电镀溶液中的一对电极提供能量输入来启动目标成分的电分析测量循环。输入到该对电极的能量被提供至少一个对应于电分析测量周期达到稳态条件的时间段的预定时间段。在随后的步骤中，在电分析测量循环达到稳态条件之后，进行电分析技术的能量输出的电分析测量。然后使用电分析测量来确定电镀溶液中的目标成分的量。在<？delete-start id =“DEL-S-00001”date =“20060110”→> close <？delete-end id =“中包括上述方法和/或一个或多个已知的电分析技术的自动计量系统 DEL-S-00001“？> <？insert-start id =”INS-S-00001“date =”20060110“？> closed <？insert-end id =”INS-S-00001“？也阐述了。

29. 发明授权

US5390531A Leak testing 失效
标题翻译：泄漏测试
公开(公告)号：US5390531A
公开(公告)日：1995-02-21
申请号：US232077
申请日：1994-04-26
申请人： Thomas C. Taylor
发明人： Thomas C. Taylor
IPC分类号： G01M3/04 , G01M3/12 , G01M3/20 , B32B3/26
CPC分类号： G01M3/04 , Y10T428/24826
摘要： An apparatus for leak testing a garment, such as an over-water flying suit formed of a waterproof material, comprises a closure plug (4) for closing the neck of the garment and clamps (36, 38, 40, 42) for holding it in place. Clamps (26, 28) close other openings in the garment to allow it to be inflated, usually turned inside out to simulate exposure to water immersion. A mixture of water and compressed air is sprayed into the inflated garment via nozzles (18). The inflated garment is then inspected visually for leaks, and may be raised to an upright position to facilitate inspection. A restraining cage (70) can be used to prevent damage by stretching during inflation.
摘要翻译： PCT No.PCT / GB92 / 02060 Sec。 371日期：1994年3月26日 102（e）1994年3月26日PCT 1992年11月9日PCT公布。出版物WO93 / 09418 日期：1993年5月13日。一种用于泄漏测试的装置，例如由防水材料形成的水上飞行服装，包括用于封闭衣服颈部的闭合塞（4）和夹具（36,38,40 ，42）将其保持在适当位置。夹子（26,28）关闭衣服中的其他开口以允许其充气，通常内翻以模拟暴露于水浸。通过喷嘴（18）将水和压缩空气的混合物喷射到充气的衣服中。然后，充气的衣服目视检查以进行泄漏，并且可以升高到直立位置以便于检查。可以使用约束笼（70）来防止在充气期间由拉伸造成的损坏。

30. 发明授权

US5385634A Sealed self aligned contact process 失效
标题翻译：密封自对准接触过程
公开(公告)号：US5385634A
公开(公告)日：1995-01-31
申请号：US43569
申请日：1993-04-07
申请人： Douglas Butler , E. Henry Stevens , Richard A. Bailey , Thomas C. Taylor
发明人： Douglas Butler , E. Henry Stevens , Richard A. Bailey , Thomas C. Taylor
IPC分类号： H01L21/28 , H01L21/285 , H01L21/3213 , H01L21/336 , H01L21/60 , H01L21/768 , H01L23/485 , H01L29/78 , H01L21/00
CPC分类号： H01L21/76897 , H01L21/28512 , H01L21/76804 , H01L23/485 , H01L2924/0002 , Y10S438/97
摘要： In fabricating a contact window to source/drain electrode next to a gate electrode of an integrated circuit: (1) establishing a structure with a window over the source/drain region next to the gate electrode; (2) establishing a region of titanium silicide over the source/drain electrode and establishing a titanium nitride layer over the window and gate electrode; (3) establishing a layer of silicon nitride over the titanium nitride layer; (4) patterning the silicon nitride layer; (5) using the patterned silicon nitride layer as a mask to pattern the titanium nitride layer; (6) adding another silicon nitride layer to seal the gate electrode where it is not protected by titanium nitride; (7) opening a window over the electrode by an anisotropic etch; (8) widening the window with an isotropic etch, using the silicon nitride and titanium nitride as a protective barrier; and (9) adding contact material in said windows.
摘要翻译：在制造与集成电路的栅电极相邻的源极/漏电极的接触窗口时：（1）在栅电极旁边的源极/漏极区域上建立具有窗口的结构; （2）在源/漏电极上建立硅化钛区域，并在窗口和栅电极上建立氮化钛层; （3）在氮化钛层上建立氮化硅层; （4）构图氮化硅层; （5）使用图案化氮化硅层作为掩模来图案化氮化钛层; （6）添加另一个氮化硅层以密封其不受氮化钛保护的栅电极; （7）通过各向异性蚀刻在电极上打开窗口; （8）使用氮化硅和氮化钛作为保护屏障，用各向同性蚀刻来加宽窗口; 和（9）在所述窗口中添加接触材料。

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