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1. 发明授权

US08550406B2 Spacecraft magnetic shield 有权
标题翻译：航天器磁盾
公开(公告)号：US08550406B2
公开(公告)日：2013-10-08
申请号：US13134733
申请日：2011-06-15
申请人： Robert T. Bigelow
发明人： Robert T. Bigelow
IPC分类号： B64G1/52
CPC分类号： B64G1/54
摘要： A spacecraft magnetic shield apparatus is disclosed. One embodiment has an armature attached at one end of a spacecraft and an electromagnet attached to the other end. A computer determines the position of the armature and electromagnet in relation to the spacecraft, and a power source powers the electromagnet. In operation, the positioning of the electromagnet is generally in line with incoming charged particles or ion radiation and powering of the electromagnet creates a magnetic field that deflects a percentage of the incoming charged particles or ion radiation from directly impacting the spacecraft.
摘要翻译：公开了一种航天器磁屏蔽装置。一个实施例具有附接在航天器的一端的电枢和附接到另一端的电磁体。计算机确定电枢和电磁体相对于航天器的位置，电源为电磁铁供电。在操作中，电磁铁的定位通常与进入的带电粒子或离子辐射一致，并且电磁铁的供电产生磁场，其使进入的带电粒子或离子辐射的百分比偏转直接影响到航天器。

2. 发明申请

US20120318928A1 Spacecraft magnetic shield 有权
标题翻译：航天器磁盾
公开(公告)号：US20120318928A1
公开(公告)日：2012-12-20
申请号：US13134733
申请日：2011-06-15
申请人： Robert T. Bigelow
发明人： Robert T. Bigelow
IPC分类号： B64G1/54 , B64G1/52
CPC分类号： B64G1/54
摘要： A spacecraft magnetic shield apparatus is disclosed. One embodiment has an armature attached at one end of a spacecraft and an electromagnet attached to the other end. A computer determines the position of the armature and electromagnet in relation to the spacecraft, and a power source powers the electromagnet. In operation, the positioning of the electromagnet is generally in line with incoming charged particles or ion radiation and powering of the electromagnet creates a magnetic field that deflects a percentage of the incoming charged particles or ion radiation from directly impacting the spacecraft.
摘要翻译：公开了一种航天器磁屏蔽装置。一个实施例具有附接在航天器的一端的电枢和附接到另一端的电磁体。计算机确定电枢和电磁体相对于航天器的位置，电源为电磁铁供电。在操作中，电磁铁的定位通常与进入的带电粒子或离子辐射一致，并且电磁铁的供电产生磁场，其使进入的带电粒子或离子辐射的百分比偏转直接影响到航天器。

3. 发明授权

US06467221B1 Spacecraft sleeping berth 有权
标题翻译：航天器睡眠泊位
公开(公告)号：US06467221B1
公开(公告)日：2002-10-22
申请号：US09644935
申请日：2000-08-23
申请人： Robert T. Bigelow
发明人： Robert T. Bigelow
IPC分类号： E04B134
CPC分类号： B64D11/00 , B64D11/0023 , B64D11/0604
摘要： The present invention provides an improved sleeping berth for space modules that can be expanded from a collapsed position to provide greater passenger comfort in a larger living space. The extension of the berth is accomplished using expandable gas inflated bellows between two hard surface housings. The berth can be retracted into its closed position simply by removing the air pressure from the bellows. The berth's retracted position may still accommodate a passenger and may be used in this position when space is unavailable for the berth's extension.
摘要翻译：本发明提供了一种用于空间模块的改进的卧铺，其可以从折叠位置扩展，以在较大的生活空间中提供更大的乘客舒适度。泊位的延伸使用两个硬表面外壳之间的可膨胀气体充气波纹管实现。通过从波纹管中除去空气压力，可以将泊位缩回到其关闭位置。泊位的缩回位置可能仍然容纳乘客，并且当空间不可用于泊位的延伸时可以用于该位置。

4. 发明授权

US06293500B1 Integrated translation tube assembly for a space module 有权
标题翻译：用于空间模块的集成平移管组件
公开(公告)号：US06293500B1
公开(公告)日：2001-09-25
申请号：US09549624
申请日：2000-04-14
申请人： Robert T. Bigelow
发明人： Robert T. Bigelow
IPC分类号： B64G110
CPC分类号： B64G1/12 , B64G9/00 , B64G2001/224
摘要： The present invention provides an improved integrated translation tube for the movement of equipment and personnel through space modules, particularly for non-rigid type space modules such as the NASA Transhab module. In addition, the present invention provides an internal framework for the structural support of the space module itself, and the equipment installed internally to the space module. The present invention's arched shaped translation tube provides sufficient strength and rigidity to provide the required structural support, while simultaneously maximizing the uninterrupted interior volume of the space module.
摘要翻译：本发明提供了一种改进的集成平移管，用于通过空间模块移动设备和人员，特别是用于非刚性型空间模块，例如NASA Transhab模块。此外，本发明提供了用于空间模块本身的结构支撑的内部框架，以及安装在空间模块内部的设备。本发明的拱形平移管提供足够的强度和刚性以提供所需的结构支撑，同时最大化空间模块的不间断的内部体积。

5. 发明授权

US09327848B2 Method of deploying a spacecraft shield in space 有权
标题翻译：在太空中部署航天器护罩的方法
公开(公告)号：US09327848B2
公开(公告)日：2016-05-03
申请号：US13507179
申请日：2012-06-11
申请人： Robert T. Bigelow
发明人： Robert T. Bigelow
IPC分类号： B64G1/56 , B82Y30/00
CPC分类号： B64G1/56 , B82Y30/00 , B82Y40/00 , Y10S977/742 , Y10S977/842 , Y10S977/902
摘要： A shield comprised of carbon nanotube materials is used to provide a level of protection to a spacecraft. Shield segments are produced in a facility in space. The segments are transported from the facility to a vicinity of a spacecraft hull. The segments are assembled over the hull to substantially cover an area of the hull.
摘要翻译：使用由碳纳米管材料组成的屏蔽罩来为航天器提供一定程度的保护。盾构段在空间设施中生产。这些段从设施运送到航天器船体附近。这些段被组装在船体上以基本上覆盖船体的区域。

6. 发明授权

US07780118B2 Radiation shield 有权
标题翻译：辐射盾
公开(公告)号：US07780118B2
公开(公告)日：2010-08-24
申请号：US10901874
申请日：2004-07-29
申请人： Robert T. Bigelow
发明人： Robert T. Bigelow
IPC分类号： B64G1/36
CPC分类号： B64G1/54
摘要： A radiation shield for use with a manned spacecraft is claimed. The shield has a container that is substantially filled with a substantially radiation absorbing material. The container has attachment members that cooperate with corresponding attachment members on the inner surface of a spacecraft. The radiation absorbing material provides a measure of protection to crewmembers and equipment against particle radiation that is present in space.
摘要翻译：要求使用与载人航天器一起使用的辐射屏蔽。屏蔽件具有基本上填充有基本上辐射吸收材料的容器。容器具有与航天器的内表面上的相应附接构件配合的附接构件。放射线吸收材料提供了防止船员和设备抵御空间中存在的颗粒辐射的措施。

7. 发明申请

US20080230655A1 Air barrier for use with an expandable structure 有权
标题翻译：用于可扩展结构的空气屏障
公开(公告)号：US20080230655A1
公开(公告)日：2008-09-25
申请号：US11723237
申请日：2007-03-19
申请人： Robert T. Bigelow
发明人： Robert T. Bigelow
IPC分类号： B64G1/00
CPC分类号： B64F1/02
摘要： An air barrier having a scuff coating is used in connection with the core of a spacecraft to form an inflatable, or expandable, human habitat module. The air barrier is comprised of a number of segments joined together to form a enclosure that has at least one opening. The joined segments are generally gas impermeable, flexible, and have a scuff coating on both sides of the segments.
摘要翻译：与空中飞行器的核心结合使用具有防刮涂层的空气屏障，以形成可膨胀或可扩张的人类栖息地模块。空气障碍物由多个段连接在一起以形成具有至少一个开口的外壳。连接的段通常是气体不可渗透的，柔性的，并且在段的两侧具有刮擦涂层。

8. 发明授权

US07309049B2 Orbital debris shield 有权
标题翻译：轨道碎片盾
公开(公告)号：US07309049B2
公开(公告)日：2007-12-18
申请号：US11498659
申请日：2006-08-03
申请人： Robert T. Bigelow
发明人： Robert T. Bigelow
IPC分类号： B64G1/56
CPC分类号： B64G1/56 , Y10T428/192
摘要： An orbital debris shield for protecting the hull of a spacecraft. The shield is comprised of a number of flexible and releasably attached gores that substantially cover the hull. Interleafed between layers of the gores are layers of a spacing material. As debris collides with the gores, the material is shocked and breaks up to some degree. As the shocked debris disperses through a layer of the gore, the spacing material interacts with the debris. After dispersing through a number of layers of the gores and the spacing material, the debris transfers a significant portion of kinetic energy and the probability of the remaining particles piercing the hull is significantly decreased.
摘要翻译：用于保护航天器船体的轨道碎片盾。护罩由许多基本上覆盖船体的柔性和可释放地附接的山脉组成。沟渠层之间的交错是间隔材料层。随着碎屑与山羊碰撞，材料受到震动，并在一定程度上破裂。当震动的碎屑通过一层玻璃分散时，间隔材料与碎屑相互作用。在分散通过多个层和间隔材料之后，碎屑转移了大部分动能，并且剩余的颗粒穿透船体的可能性显着降低。

9. 发明授权

US07100874B2 Flexible structural restraint layer for use with an inflatable modular structure 有权
标题翻译：柔性结构约束层，用于充气模块化结构
公开(公告)号：US07100874B2
公开(公告)日：2006-09-05
申请号：US10722904
申请日：2003-11-25
申请人： Robert T. Bigelow , Aiken Brian
发明人： Robert T. Bigelow , Aiken Brian
IPC分类号： E04B1/34 , B64G1/12
CPC分类号： B29C70/222 , B29L2031/7156
摘要： A flexible structural restraint layer for use with an inflatable modular structure, having a fore and aft assembly separated by a longeron and an inflatable bladder. The restraint layer is comprised of two circumferential strap assemblies, each attachedly fastened at opposing ends of a radial strap assembly. There are a plurality of axial straps that are secured in place to the circumferential strap assemblies and the radial strap assembly. The restraint layer surrounds the bladder and the ends of the axial straps are secured in place at the fore and aft end of the modular structure. When the bladder is inflated, the structural restraint layer distributes the load created by the inflated bladder.
摘要翻译：一种用于可充气模块化结构的柔性结构约束层，具有由龙门和可膨胀囊隔开的前后组件。约束层由两个周向带组件组成，每个带状组件分别紧固在径向带组件的相对端。存在多个轴向带，其固定到周边带组件和径向带组件的适当位置。约束层围绕囊，并且轴向带的端部固定在模块化结构的前端和后端的适当位置。当膀胱膨胀时，结构约束层分布由膨胀的膀胱产生的负荷。

10. 发明授权

US06962310B1 Inflatable satellite bus 有权
标题翻译：充气卫星总线
公开(公告)号：US06962310B1
公开(公告)日：2005-11-08
申请号：US10981195
申请日：2004-11-04
申请人： Robert T. Bigelow
发明人： Robert T. Bigelow
IPC分类号： B64G1/00 , B64G1/10 , B64G1/12 , B64G1/42 , B64G1/44 , B64G1/56
CPC分类号： B64G1/10 , B64G1/1007 , B64G1/1021 , B64G1/12 , B64G1/422 , B64G1/423 , B64G1/443 , B64G1/56 , B64G2001/224
摘要： An inflatable satellite bus is claimed for use with a mission payload. The inflatable satellite bus is comprised of a core adapted to receive a mission payload. There is an expandable shell attached to the core and substantially enclosing the core. The core has an attitude control device and a power system attached to the core and operated by a controller.
摘要翻译：声称使用充气卫星总线与任务有效载荷一起使用。充气卫星总线由适于接收任务负载的核心组成。有一个可扩展的外壳，连接在芯上并且基本上包围着芯。核心具有姿态控制装置和附接到核心并由控制器操作的电力系统。

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