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1. 发明授权

US07562670B1 Flat valve for orbital applications 有权
标题翻译：用于轨道应用的扁平阀
公开(公告)号：US07562670B1
公开(公告)日：2009-07-21
申请号：US11412786
申请日：2006-04-28
申请人： H. Stephen Jones , Walter P. Kistler , Thomas C. Taylor
发明人： H. Stephen Jones , Walter P. Kistler , Thomas C. Taylor
IPC分类号： F16K17/40
CPC分类号： F16K17/40 , Y10T137/1767 , Y10T137/6123
摘要： A thin diaphragm valve includes a base plate attached to a valve attach plate. A diaphragm is positioned between the plates to move between open and closed positions. A spring can be provided between the diaphragm and a sealing flange of a pipe. Because no sliding friction occurs between sealing surfaces, wear is reduced and leakage is also reduced. A pierceable membrane can also be added to provide additional security.
摘要翻译：薄隔膜阀包括附接到阀附接板的基板。隔板位于板之间，以在打开和关闭位置之间移动。可以在隔膜和管道的密封凸缘之间设置弹簧。由于密封面之间不产生滑动摩擦，所以磨损减少，泄漏也减少。也可以添加可刺破的膜以提供额外的安全性。

2. 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。

3. 发明授权

US07118077B1 Platform and system for mass storage and transfer in space 有权
标题翻译：空间大容量存储和传输的平台和系统
公开(公告)号：US07118077B1
公开(公告)日：2006-10-10
申请号：US11076950
申请日：2005-03-11
申请人： Walter P. Kistler , Robert A. Citron , Thomas C. Taylor
发明人： Walter P. Kistler , Robert A. Citron , Thomas C. Taylor
IPC分类号： B64G1/00
CPC分类号： B64G1/646 , B64G1/1078
摘要： A platform for storage and transfer of payloads in space includes a plate for supporting a payload, and a transfer mechanism for transferring the payload to and from the plate. A groove extends diametrically between two edges of the plate for receiving a rail provided on the payload. The rail includes a plurality of teeth, and the transfer mechanism includes a gear which interacts with the teeth for moving the rail. Two platforms may be positioned adjacent to each other for transferring a payload. Docking of the two platforms includes engagement of tapered pins and tapered holes on the platforms. In this manner, the grooves of the platforms are aligned. The rail is passed between the grooves of the platforms for transferring the payload between the platforms.
摘要翻译：用于存储和传送空间中的有效载荷的平台包括用于支撑有效载荷的板，以及用于将载荷传递到板的转移机构。凹槽在板的两个边缘之间径向延伸，用于接收设置在有效载荷上的导轨。轨道包括多个齿，并且传送机构包括与齿啮合的齿轮，用于移动轨道。两个平台可以彼此相邻地定位以传送有效载荷。两个平台的对接包括平台上的锥形销和锥形孔的接合。以这种方式，平台的凹槽对齐。轨道在平台的槽之间通过，用于在平台之间传送有效载荷。

4. 发明授权

US07114682B1 System and method for transportation and storage of cargo in space 有权
标题翻译：空运货物的运输和储存系统和方法
公开(公告)号：US07114682B1
公开(公告)日：2006-10-03
申请号：US10862604
申请日：2004-06-07
申请人： Walter P. Kistler , Robert A. Citron , Thomas C. Taylor
发明人： Walter P. Kistler , Robert A. Citron , Thomas C. Taylor
IPC分类号： B64G1/64
CPC分类号： B64G1/402 , B64G1/242 , B64G1/26 , B64G1/40 , B64G1/401 , B64G1/54 , B64G1/646 , B64G2004/005
摘要： A system for transportation and storage of cargo in space includes one or more platforms. The platforms are operable to hold multiple removable propellant tanks and rendezvous with one or more other platforms in space. The platforms also include one or more thruster systems and positioners. Each positioner has an effector operable to grip a band disposed around each propellant tank. Each positioner is operable to facilitate the transfer of the multiple removable propellant tanks between platforms during the rendezvous.
摘要翻译：空运货物的运输和储存系统包括一个或多个平台。这些平台可操作以容纳多个可拆卸的推进剂罐并与空间中的一个或多个其他平台会合。平台还包括一个或多个推进器系统和定位器。每个定位器具有可操作地抓握设置在每个推进剂罐周围的带的效应器。每个定位器可操作以便于在会合期间在平台之间传送多个可拆卸的推进剂罐。

5. 发明授权

US07503526B1 Space transportation node including tether system 有权
标题翻译：空间运输节点包括系绳系统
公开(公告)号：US07503526B1
公开(公告)日：2009-03-17
申请号：US11232932
申请日：2005-09-23
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： B64G1/28
CPC分类号： B64G1/34 , B64G1/002 , B64G1/12 , B64G1/14 , B64G1/402 , B64G1/50 , B64G1/62 , B64G1/646 , B64G1/648
摘要： A transportation node system orbits a celestial body. The node system includes a truss having two ends, the truss rotating around its center of mass while orbiting the celestial body. The truss stores payloads. The node system also includes tether tips, each attached to one end of the truss via a tether so that each tether tip can extend from the truss and retract to the truss for transfer of payloads. The tether runs through the length of the truss and connects to each tether tip, each tether tip being capable of engaging payloads. The node further includes at least one tether cable reel that reels in and reels out the tether so the tether tips can extend from and retract to the truss.
摘要翻译：运输节点系统绕着天体。节点系统包括具有两端的桁架，桁架围绕其中心旋转，同时绕着天体转动。桁架存储有效载荷。节点系统还包括系绳末端，每个系绳尖通过系绳连接到桁架的一端，使得每个系绳尖端可以从桁架延伸并缩回到桁架以传送有效载荷。系绳穿过桁架的长度并连接到每个系绳尖端，每个系绳尖端能够接合有效载荷。节点还包括至少一个系绳电缆卷轴，其卷绕并卷出系绳，使得系绳尖端可以从桁架延伸并缩回到桁架。

6. 发明授权

US07156348B1 Platform and system for propellant tank storage and transfer in space 有权
标题翻译：推进剂罐储存和空间转移的平台和系统
公开(公告)号：US07156348B1
公开(公告)日：2007-01-02
申请号：US11076926
申请日：2005-03-11
申请人： Walter P. Kistler , Robert A. Citron , Thomas C. Taylor
发明人： Walter P. Kistler , Robert A. Citron , Thomas C. Taylor
IPC分类号： B64G1/64
CPC分类号： B64G1/402 , B64G1/1078 , B64G1/26 , B64G1/401 , B64G1/646 , F17C13/088 , F17C2201/0104 , F17C2205/0107 , F17C2205/013 , F17C2205/032 , F17C2205/0364 , F17C2205/0376 , F17C2221/011 , F17C2221/012 , F17C2223/0161 , F17C2223/033 , F17C2270/0194 , Y02E60/321
摘要： A platform for storage and transfer of propellant tanks in space includes frames configured to releasably support plural propellant tanks in storage positions, and transfer mechanisms configured to transfer propellant tanks to and from the storage positions. The platform includes a central structure to which the plural frames are connected at predetermined spaced intervals. The transfer mechanisms include extendable telescoping arms mounted to the central structure. The arms have end effectors configured to grip bands on propellant tanks. Two platforms may be positioned adjacent each other for the transfer of propellant tanks therebetween.
摘要翻译：用于在空间中存储和传送推进剂罐的平台包括被配置为将多个推进剂罐可释放地支撑在储存位置的框架，以及构造成将推进剂罐传送到存储位置和从储存位置传送推进剂罐的传送机构。平台包括以预定间隔的间隔连接多个框架的中心结构。传送机构包括安装在中央结构上的伸缩臂。臂具有构造成抓住推进剂罐上的带的末端效应器。两个平台可以彼此相邻地定位以在其间传送推进剂罐。

7. 发明授权

US07681840B1 Space transportation node including tether system 有权
标题翻译：空间运输节点包括系绳系统
公开(公告)号：US07681840B1
公开(公告)日：2010-03-23
申请号：US12331311
申请日：2008-12-09
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： B64G1/28
CPC分类号： B64G1/34 , B64G1/002 , B64G1/12 , B64G1/14 , B64G1/402 , B64G1/50 , B64G1/62 , B64G1/646 , B64G1/648
摘要： A transportation node that orbits a celestial body includes a truss having two ends with least at one end of the truss having at least one coupling tether cable with a tether tip at individual ends. The truss, while orbiting the celestial body, rotates around its center of mass in a direction to control the tether tip in relation to a surface of the celestial body and to cancel a relative velocity between the tether tip and the surface for transferring a payload attached to the tether tip to and from the surface. A method of transferring payload to and from a celestial body includes reeling in/out from an orbiting transportation node a coupling tether cable with a tether tip configured to attach to the payload.
摘要翻译：围绕天体的运输节点包括具有两端的桁架，桁架的一端的至少一端具有至少一个连接系绳，在单个端部具有系绳末端。桁架在绕着天体的同时围绕其质心旋转，以相对于天体的表面控制系绳末端，并且消除系绳末端和表面之间的相对速度以传递附着的有效载荷连接到表面上的绳索尖端。将有效负载传送到天体的方法包括从轨道运输节点卷入/离开具有配置为附接到有效载荷的系绳末端的耦合系绳电缆。

8. 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。

9. 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。

10. 发明申请

US20090127399A1 SYSTEM FOR USE OF EXTERNAL SECONDARY PAYLOADS 审中-公开
标题翻译：使用外部二次付费的系统
公开(公告)号：US20090127399A1
公开(公告)日：2009-05-21
申请号：US11955612
申请日：2007-12-13
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： B64G1/62 , B64G1/00 , B64G1/40
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. 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。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。

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