专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

11. 发明授权

US06206328B1 Centrifugal gravity habitation torus constructed of salvaged orbital debris 失效
标题翻译：离心式重力居住环形构造由抢救的轨道碎片
公开(公告)号：US06206328B1
公开(公告)日：2001-03-27
申请号：US09188076
申请日：1998-11-09
申请人： Thomas C. Taylor
发明人： Thomas C. Taylor
IPC分类号： B64G156
CPC分类号： B64G1/60 , B64G1/12 , B64G1/56 , B64G1/64
摘要： An aerospace hardware derelict item is salvaged in space, modified, and reused to provide manned facilities in orbit. The hardware packages added onto the salvaged discarded item enhances its value, and incorporates at least the subsystems required to effectively reuse portions of previously discarded launch vehicle components, and other derelict objects in space. The hardware, and technique used reduces the cost of launching comparable hardware to orbit, because of the reuse, and provides a human habitation in orbit. The salvaged items include the external tank of the space shuttle, other derelict orbital hardware, the add-on cargo pod in two forms, and the ability to convert the derelict into a cost effective reusable item. The salvaged hardware is initially capable of contributing mass, length, interior volume, strongback, rotational stability mass, interior pressurized volumes, artificial gravity, and stability with the addition of simple subsystems for salvage, and interior development packages.
摘要翻译：航空硬件废弃物在空间中被抢救，修改和重用，以便在轨道上提供载人设施。添加到被抢救的丢弃物品上的硬件包增强了其价值，并且至少包含了有效地重用先前丢弃的运载火箭部件的部分和空间中的其他废弃物体所需的子系统。使用的硬件和技术降低了将可比较的硬件发射到轨道的成本，因为重用，并提供了人造卫星的轨道。抢救项目包括航天飞机的外部坦克，其他废弃轨道硬件，两种形式的附加货物舱，以及将遗弃物转化为成本有效的可重复使用物品的能力。抢救的硬件最初能够通过添加简单的辅助子系统和内部开发包来提供质量，长度，内部体积，强度，旋转稳定性质量，内部加压体积，人造重力和稳定性。

12. 发明授权

US4650139A Aerospike for attachment to space vehicle system 失效
公开(公告)号：US4650139A
公开(公告)日：1987-03-17
申请号：US636292
申请日：1984-07-31
申请人： Thomas C. Taylor , Peter Cerna
发明人： Thomas C. Taylor , Peter Cerna
IPC分类号： B64C1/38 , B64G1/14 , B64G1/64 , B64G1/52
CPC分类号： B64C1/38 , B64C23/04 , B64G1/14
摘要： An aerospike is adapted to be attached to the front nose of an aerodynamically asymmetric space vehicle system, such as the external tank and orbiter of the space shuttle. The aerospike basically comprises a tapered elongated portion having a first end which is adapted to be attached to the nose of the space vehicle, and a second free end terminating in a substantially rounded disc-like tip member. Use of the spike reduces aerodynamic heating and drag during ascent of the space vehicle into its orbital position, provides an attachment point for tether operations and for propellant recovery, and permits transportion of an external tank into its orbit.

13. 发明授权

US4562979A Expandable spacecraft 失效
标题翻译：可扩展航天器
公开(公告)号：US4562979A
公开(公告)日：1986-01-07
申请号：US477482
申请日：1983-03-21
申请人： Thomas C. Taylor
发明人： Thomas C. Taylor
IPC分类号： B64G1/12 , B64G99/00
CPC分类号： B64G9/00 , B64G1/12
摘要： An expandable spacecraft is provided which includes at least one main generally cylindrical body member. This body member comprises a generally waffle-type structure which includes a plurality of flanges extending generally radially from the body member. An auxiliary housing is provided which is adapted to increase the volume of the body member. The auxiliary housing is connected to the main body member and is slidably and telescopically received therein. The main body portion and auxiliary housing member can be provided in a compact state with a predetermined volume or can be expanded by extending the housing outwardly from the main body member to increase the volume of the assembly to a desired degree.
摘要翻译：提供了一种可扩展的航天器，其包括至少一个主要大致圆柱形的本体构件。该主体构件包括通常为华夫饼型结构，其包括从主体构件大致径向延伸的多个凸缘。提供辅助壳体，其适于增加主体构件的体积。辅助壳体连接到主体构件并且可滑动地和可伸缩地容纳在其中。主体部分和辅助壳体构件可以以预定体积的紧凑状态设置，或者可以通过将壳体从主体构件向外延伸而扩展，从而将组件的体积增加到期望的程度。

14. 发明授权

US07354020B2 System for use of external secondary payloads 失效
标题翻译：使用外部辅助有效载荷的系统
公开(公告)号：US07354020B2
公开(公告)日：2008-04-08
申请号：US10698261
申请日：2003-10-31
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： B64G1/22
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。

15. 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。

16. 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。

17. 发明授权

US5813632A Salvage hardware apparatus and method for orbiting objects 失效
标题翻译：用于轨道物体的救助硬件装置和方法
公开(公告)号：US5813632A
公开(公告)日：1998-09-29
申请号：US537531
申请日：1995-10-02
申请人： Thomas C. Taylor
发明人： Thomas C. Taylor
IPC分类号： B64G1/00 , B64G1/12 , B64G1/64 , B64G99/00
CPC分类号： B64G1/646 , B64G1/12 , B64G1/002 , B64G9/00
摘要： An aerospace hardware package is used to salvage derelicts in space. The package incorporates at least the subsystems required to salvage and reuse portions of previously discarded launch vehicle components and other derelict objects in space. The salvaged items include the external tank of the space shuttle, and the Russian-made ENERGIA rocket system in two forms. The salvaged hardware is capable of contributing mass, length, exterior surface, strongback, gravity gradient stability, interior volumes, base metal sources and stability with the addition of a salvage subsystems package. The package supplies capabilities such as power and communications and later evolves toward more complex services taking full advantage of the salvaged hardware's attributes to reduce the cost and difficulty of space operations.
摘要翻译：使用航空硬件包来拯救空间中的遗弃物。该包装至少包含了以前废弃的运载火箭部件和空间中其他遗弃物体的部分补救和再利用所需的子系统。抢救项目包括航天飞机的外部坦克和俄制的能源火箭系统两种形式。通过添加补救子系统，经过回收的硬件能够提供质量，长度，外表面，强力，重力梯度稳定性，内部体积，贱金属源和稳定性。该软件包提供诸如电力和通信的功能，并且随后演变成更复杂的服务，充分利用被抢救的硬件属性来降低空间操作的成本和难度。

18. 发明授权

US4790499A Aerospike for attachment to space vehicle system 失效
标题翻译：太空飞船用于附加到太空车系统
公开(公告)号：US4790499A
公开(公告)日：1988-12-13
申请号：US925290
申请日：1986-10-31
申请人： Thomas C. Taylor , Peter Cerna
发明人： Thomas C. Taylor , Peter Cerna
IPC分类号： B64C1/38 , B64G1/14 , B64G1/64
CPC分类号： B64C1/38 , B64C23/04 , B64G1/14
摘要： An aerospike is adapted to be attached to the front nose of an aerodynamically asymmetric space vehicle system, such as the external tank and orbiter of the space shuttle. The aerospike basically comprises a tapered elongated portion having a first end which is adapted to be attached to the nose of the space vehicle, and a second free end terminating in a substantially rounded disc-like tip member. Use of the spike reduces aerodynamic heating and drag during ascent of the space vehicle into its orbital position, provides an attachment point for tether operations and for propellant recovery, and permits transportion of an external tank into its orbit.
摘要翻译：气垫适合附着在空气动力学不对称空间车辆系统的前鼻部，例如外部舱和航天飞机的轨道飞行器。气枪基本上包括锥形细长部分，其具有适于附接到空间车辆的鼻部的第一端和终止于基本上圆形的盘状尖端部件的第二自由端。使用尖钉可以减少空中交通工具进入其轨道位置时的空气动力学加热和阻力，为系绳操作和推进剂回收提供附着点，并允许外部油箱进入其轨道。

19. 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。

20. 发明授权

US06439508B1 Inflatable habitation volumes in space 有权
标题翻译：空间充气居住体积
公开(公告)号：US06439508B1
公开(公告)日：2002-08-27
申请号：US09686145
申请日：2000-10-10
申请人： Thomas C. Taylor
发明人： Thomas C. Taylor
IPC分类号： B64G110
CPC分类号： B64G1/60 , B64G1/12 , B64G1/56 , B64G1/641 , B64G2001/224
摘要： An improved inflatable habitation volume in space comprising reduced cost, improved debris impact protection, enhanced penetration resistance, self sealing qualities, innovative flat end caps, industry accepted commercial design/manufacturing techniques, enhanced inflatable assembly techniques and expanded interior volume. Costs are reduced by compressing the launch package, removing the three gravity launch load requirements from the transportation process and inflating in microgravity. The inflatable habitation volume unit can be connected to either existing orbital facilities or connected to similar units to create expanded volumes and space tourist torus structures rotated for partial gravity.
摘要翻译：空间中的改善的充气居住体积包括降低的成本，改进的碎片冲击保护，增强的穿透阻力，自密封性质，创新的扁平端盖，业界公认的商业设计/制造技术，增强的充气组装技术和扩大的内部容积。通过压缩发射包降低成本，消除运输过程中的三个重力发射载荷要求，并在微重力中膨胀。可充气居住体积单元可以连接到现有的轨道设施或连接到类似的单元，以产生扩展的体积和空间的旅游环形结构旋转以进行部分重力。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式