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1. 发明授权

US10011372B2 Systems and methods for shielding structures from radiation and magnetic field exposure 有权
公开(公告)号：US10011372B2
公开(公告)日：2018-07-03
申请号：US14926669
申请日：2015-10-29
申请人： THE BOEING COMPANY
发明人： Jian Dong , Naveed Moayyed Hussain
IPC分类号： B64G1/00 , B64G1/54 , B64G1/52
CPC分类号： B64G1/543 , B64G1/12 , B64G1/546 , B64G2001/525
摘要： A system is configured to shield an interior chamber of a structure. The system may include a power source, an outer shield assembly operatively connected to the power source and coupled to an outer wall of the structure, and an inner shield assembly surrounding the internal chamber. The outer shield assembly generates a magnetic field through and around the structure. The inner shield assembly deflects radiation particles away from the interior chamber and re-directs portions of the magnetic field around the interior chamber.

2. 发明申请

US20170197736A1 GRAVITY CHAMBER FOR A HABITATION MODULE THAT ROTATES ON SUPPORT BEARINGS 审中-公开
公开(公告)号：US20170197736A1
公开(公告)日：2017-07-13
申请号：US14992946
申请日：2016-01-11
申请人： The Boeing Company
发明人： Raju Dharmaraj , James Michael Engle , Patrick A. Swartzell , Karl David Heiman , Travis Andrew Moseman
IPC分类号： B64G1/60 , B64G1/46
CPC分类号： B64G1/60 , B64G1/12 , B64G1/46
摘要： A habitation module with a gravity chamber that provides an artificial gravity environment. In one embodiment, the gravity chamber is annular and includes an outer cylindrical wall, an inner cylindrical structure, and opposing side walls that connect the outer cylindrical wall and the inner cylindrical structure. The gravity chamber attaches to a cylindrical core member of the habitation module with support bearings. The support bearing includes an inner race attached to the cylindrical core member, and an outer race attached to the gravity chamber. A drive mechanism drives the outer race of the support bearing to rotate the gravity chamber about an axis to simulate a gravitational force within the gravity chamber.

3. 发明申请

US20170197734A1 PORTAL CHAMBER FOR ENTERING OR EXITING A GRAVITY CHAMBER OF A HABITATION MODULE WHILE THE GRAVITY CHAMBER ROTATES 审中-公开
公开(公告)号：US20170197734A1
公开(公告)日：2017-07-13
申请号：US14992965
申请日：2016-01-11
申请人： The Boeing Company
发明人： Raju Dharmaraj , James Michael Engle
IPC分类号： B64G1/12 , B64G1/60
CPC分类号： B64G1/12 , B64G1/46 , B64G1/60
摘要： A habitation module with a gravity chamber that rotates to provide an artificial gravity environment. In one embodiment, a portal chamber is installed adjacent to the gravity chamber and configured to rotate about the same axis. The portal chamber includes a brake mechanism to stop the rotation of the portal chamber, a first access opening for a crew member to pass between an interior of the habitation module and the portal chamber while rotation of the portal chamber is stopped, an engagement mechanism that engages the gravity chamber to rotate the portal chamber about the axis at a speed of the gravity chamber, and a second access opening for the crew member to pass between the portal chamber and the gravity chamber while the portal chamber rotates at the speed of the gravity chamber.

4. 发明申请

US20170183109A1 Multi-purpose expandable complex providing maintenance, manufacturing, assemblage complex with external space dock 审中-公开
公开(公告)号：US20170183109A1
公开(公告)日：2017-06-29
申请号：US14998744
申请日：2016-02-09
申请人： John Aylmer
发明人： John Aylmer
IPC分类号： B64G1/64 , B64G1/40 , B64G1/54 , B64G1/10 , B64G1/48 , B64G1/14
CPC分类号： B64G1/646 , B64G1/105 , B64G1/1078 , B64G1/12 , B64G1/14 , B64G1/422 , B64G1/48 , B64G1/543 , B64G4/00 , B64G2001/1064 , B64G2001/1092 , B64G2004/005
摘要： This present invention describes initial sequential methods for constructing and placing into operation a multi-purpose maintenance complex and a space dock in high geosynchronous orbit. This is dual function complex that can provide a orbital platforms to a commercial profitable enterprise or to the Department of Defense (DoD) to enhance their capabilities. A complex will have the capability to fabricate, assemble, test, and place into full operation any size orbital and planetary surface complexes and spacecraft. DoD mission capabilities embracing satellite repairs, research, national security and deterrence, space junk disposal support and other services while in orbit.

5. 发明授权

US09567114B2 Combined pressure and thermal window system for space vehicles 有权
标题翻译：太空车组合压力和热窗系统
公开(公告)号：US09567114B2
公开(公告)日：2017-02-14
申请号：US14692744
申请日：2015-04-22
申请人： The Boeing Company
发明人： Kirk Nils Svartstrom
IPC分类号： B64C1/14 , B64G1/58 , B64G1/52 , B64G1/66 , B64G1/12 , B64G1/62
CPC分类号： B64G1/58 , B64C1/1492 , B64G1/12 , B64G1/52 , B64G1/62 , B64G1/66
摘要： A window system for a vehicle comprising a pressure and thermal window pane, a seal system, and a retainer system. The pressure and thermal window pane may be configured to provide desired pressure protection and desired thermal protection when exposed to an environment around the vehicle during operation of the vehicle. The pressure and thermal window pane may have a desired ductility. The seal system may be configured to contact the pressure and thermal window pane to seal the pressure and thermal window pane. The retainer system may be configured to hold the seal system and the pressure and thermal window pane.
摘要翻译：一种用于车辆的窗系统，包括压力和热窗玻璃，密封系统和保持器系统。压力和热窗格可以被配置为当在车辆操作期间暴露于车辆周围的环境时提供期望的压力保护和期望的热保护。压力和热窗玻璃可能具有所需的延展性。密封系统可以被配置为接触压力和热窗玻璃以密封压力和热窗玻璃。保持器系统可以被配置为保持密封系统和压力和热窗玻璃。

6. 发明申请

US20160376038A1 RELEVATOR, RELEVATOR SYSTEM, AND METHOD OF USING A RELEVATOR 有权
标题翻译：相关器，相关器系统和使用相关器的方法
公开(公告)号：US20160376038A1
公开(公告)日：2016-12-29
申请号：US14747726
申请日：2015-06-23
申请人： Joseph Michael Clay
发明人： Joseph Michael Clay
IPC分类号： B64G1/60 , B64G1/14
CPC分类号： B64G1/60 , B23P17/04 , B64G1/12 , B64G1/14 , B64G1/50 , E05D15/02 , Y10T29/49716
摘要： A relevator adapted to transition an object between a stationary compartment and a rotating module rotating in a first direction, the relevator comprising: a plurality of concentric substantially solid structures separated by a plurality of concentric compartments all concentrically positioned around a central axis; a relevator central shaft extending along the central axis; the relevator being adapted to receive a rotate signal and a stop signal, one or more of the concentric compartments comprising an entry from the stationary compartment in a stop position and an entry into the rotating module in a rotating position.
摘要翻译：一种适应于在固定隔间和沿第一方向旋转的旋转模块之间转换物体的重新引导者，所述重新引导者包括：由多个同心隔间隔开的多个同心基本上实心的结构，所述多个同心隔室全部围绕中心轴同心地定位; 一个沿着中心轴延伸的再生器中心轴; 所述重新引导装置适于接收旋转信号和停止信号，所述同心隔间中的一个或多个包括处于停止位置的来自所述静止隔间的入口以及在旋转位置进入所述旋转模块。

7. 发明授权

US09045242B2 Mechanically fastened large pressurized vehicle structure 有权
标题翻译：机械固定大型加压车辆结构
公开(公告)号：US09045242B2
公开(公告)日：2015-06-02
申请号：US14058712
申请日：2013-10-21
申请人： The Boeing Company
发明人： Thomas L. Andrews
IPC分类号： B21D19/00 , B64G1/60 , B64G1/00 , F16J15/00
CPC分类号： B64G1/60 , B21D19/00 , B64G1/00 , B64G1/10 , B64G1/12 , F16J15/00 , Y10T29/49622
摘要： A first part, a second part, and a seal ring are fastened together to form a pressure structure configured for a spacecraft structure of a spacecraft, wherein the first part and the second part are each formed from a single workpiece.
摘要翻译：第一部分，第二部分和密封环被紧固在一起以形成构造成用于航天器的航天器结构的压力结构，其中第一部分和第二部分各自由单个工件形成。

8. 发明申请

US20150090841A1 Transport Landing Vehicle 有权
标题翻译：运输着陆车
公开(公告)号：US20150090841A1
公开(公告)日：2015-04-02
申请号：US14121596
申请日：2014-09-22
申请人： Bigelow Aerospace LLC
发明人： Robert T. Bigelow
IPC分类号： B64G1/26 , B64G1/60 , B64G1/40
CPC分类号： B64G1/26 , B64G1/12 , B64G1/402 , B64G1/60 , B64G2001/1071
摘要： A transport landing vehicle for transferring an astronaut to and from an extraterrestrial mass such as a moon, asteroid, or small planet is disclosed. The transport landing vehicle has a cage that is substantially open to the outside environment.
摘要翻译：公开了用于将宇航员转移到诸如月球，小行星或小行星的地球外物质的运输着陆车辆。运输着陆车具有基本上对外部环境开放的保持架。

9. 发明申请

US20150008290A1 Docking node transporter tug 有权
标题翻译：对接节点运输拖船
公开(公告)号：US20150008290A1
公开(公告)日：2015-01-08
申请号：US14120840
申请日：2014-07-02
申请人： Bigelow Aerospace LLC
发明人： Robert T. Bigelow
IPC分类号： B64G1/64 , B64G1/44 , B64G1/42 , B64G1/24 , B64G1/40
CPC分类号： B64G1/646 , B64G1/12 , B64G1/26 , B64G1/401 , B64G1/402 , B64G1/425 , B64G1/44
摘要： A docking node transporter tug is disclosed. The tug can dock with various spacecraft to allow access by people between the spacecraft. Further, the tug may dock with other specialty tugs to form a custom system.
摘要翻译：公开了一种对接节点运输拖船。拖船可以与各种航天器对接，以允许人们在飞船之间进入。此外，拖船可以与其他专业拖船对接，形成定制系统。

10. 发明授权

US08850746B2 Seal assembly with leak test components 有权
标题翻译：密封组件与泄漏测试组件
公开(公告)号：US08850746B2
公开(公告)日：2014-10-07
申请号：US12591746
申请日：2009-11-30
申请人： Lannie D. Harrison
发明人： Lannie D. Harrison
IPC分类号： B65D1/24 , G01M3/28 , B64G1/22 , B64G1/12
CPC分类号： G01M3/2869 , B64G1/12 , B64G1/22
摘要： A seal assembly is provided for maintaining a pressure difference between an exterior and an interior of an object having an access hatch and an access hatch frame. The seal assembly has a seal retainer having an interior face oriented toward the interior of the object, an exterior face oriented toward the exterior of the object, a hatch-side face oriented toward the access hatch and extending from the interior face to the exterior face, and frame-side face oriented toward the access hatch frame and extending from the interior face to the exterior face. The seal assembly also has at least one sealing member mounted on either the interior face or the exterior face of the seal retainer and a plurality of conduits formed in the seal retainer and extending from the exterior face to the interior face. The plurality of conduits include at least one supply conduit located between either the hatch-side or frame-side face and the at least one sealing member and at least one return conduit located so that the at least one sealing member is positioned between the at least one supply conduit and the at least one return conduit.
摘要翻译：提供一种密封组件，用于保持具有进入舱口和进入舱口框架的物体的外部和内部之间的压力差。密封组件具有密封保持器，其具有朝向物体内部的内表面，朝向物体外部定向的外表面，朝向入口舱口定向并从内表面延伸到外表面的舱口侧面以及朝向所述进入舱口框架定向并从所述内表面延伸到所述外表面的框架侧面。密封组件还具有安装在密封保持器的内表面或外表面上的至少一个密封构件和形成在密封保持器中并从外表面延伸到内表面的多个导管。多个管道包括位于舱口侧或框架侧面和至少一个密封构件之间的至少一个供应管道和至少一个返回管道，其至少一个密封构件位于至少一个一个供应管道和至少一个返回管道。

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