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公开(公告)号：US11884425B2
公开(公告)日：2024-01-30
申请号：US17653644
申请日：2022-03-04
发明人： Robert Weber Mah
摘要： A spacecraft capable of generating an artificial gravity environment comprises frame with a circular track with at least two modules traveling on the track. The two modules are configured to engage the first track opposite the first module to minimize mass imbalance, and a balancing system for the first and second modules configured to mass balance the first and second modules relative to each other. The frame itself does not rotate, and may have other mission supporting structures attached, including storage and supply modules, and observational modules, and spacecraft hangars and spacecraft docking modules. A method of operating a spacecraft to generate artificial gravity in a habitation module comprises operating a frame in space, propelling first and second habitation modules about the frame to generate artificial gravity environments in the modules, and mass balancing the first module relative to the second module to maintain balance of the spacecraft.
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公开(公告)号：US11780612B1
公开(公告)日：2023-10-10
申请号：US17030273
申请日：2020-09-23
摘要： A Space Traffic Management (STM) system comprising a Space Traffic Management System Service Supplier (S3) interface for sending a space conjunction request to a Conjunction Assessment Supplier (CAS) interface, and a Space Situational Awareness Supplier (SSA) interface for receiving and fulfilling space object data requests. The system further comprising the Conjunction Assessment Supplier (CAS) interface for receiving the space conjunction request from the S3 interface, requesting and receiving the space object data from the SSA interface, and generating and sending a conjunction data message to the S3 interface. The system enables coordination of an automated service for spacecraft owner operators to anticipate and avoid a space traffic conjunction using the conjunction data message.
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公开(公告)号：US11478740B2
公开(公告)日：2022-10-25
申请号：US16435984
申请日：2019-06-10
发明人： Thomas David Hanson
摘要： A filter includes a filter outer wall, and a filter inner wall spaced apart from the filter outer wall. The filter inner wall and the filter outer wall define a filter void therebetween, and the filter inner wall and the filter outer wall extend along a filter axis. A volume of filtration material is positioned in the filter void, and a plurality of baffles extend between the filter inner wall and the filter outer wall. The plurality of baffles are configured to induce a helical component to an airflow entering the filter void at a first void end relative to the filter axis and exiting the filter void at a second void end opposite the first void end.
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公开(公告)号：US20200151911A1
公开(公告)日：2020-05-14
申请号：US16729476
申请日：2019-12-29
发明人： SUQUAN DING
摘要： The automatic control method for preventing experimental data loss of space station includes: presetting shadow feature data cast by said target orbiting craft on said solar panels; detecting whether there is any target orbiting craft; acquiring a surface image of said solar panels after detecting the target orbiting craft; analyzing the acquired surface image of solar panels to detect whether there is any shadow feature data; starting power ensuring control for the environment control and life support system if the shadow feature data is detected; matching said shadow feature data with the above-mentioned preset shadow feature data cast by the target orbiting craft on said solar panels, wherein if they match each other, said experiment cabin is powered continuously to prevent data loss of the experiment cabin, which can effectively avoid unnecessary experimental data loss of the space station.
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5.发明申请公开(公告)号：US20180370661A1
公开(公告)日：2018-12-27
申请号：US15633197
申请日：2017-06-26
申请人： The Boeing Company
摘要： A habitation module that provides an artificial gravity environment. In one embodiment, the habitation module includes a rotating structure that rotates about an axis in relation to a stationary structure. The rotating structure includes a first gravity chamber that projects radially from the rotating structure, and a second gravity chamber that projects radially from the rotating structure in an opposite direction than the first gravity chamber. The first gravity chamber and the second gravity chamber are each comprised of a plurality of ring members that form side walls of the first gravity chamber and the second gravity chamber. The ring members are concentric so that the side walls of the first gravity chamber and the second gravity chamber radially extend and radially contract in upon themselves.
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公开(公告)号：US09776743B2
公开(公告)日：2017-10-03
申请号：US14992956
申请日：2016-01-11
申请人： The Boeing Company
发明人： Raju Dharmaraj , Patrick A. Swartzell , James Michael Engle , Thomas L. Hoffman , Travis Andrew Moseman , Karl David Heiman
CPC分类号： B64G1/46 , B64G1/60 , B64G2001/224
摘要： A habitation module with a gravity chamber that provides an artificial gravity environment. In one embodiment, the gravity chamber includes an inner cylindrical structure, outer wall segments that are attachable to one another to form an outer cylindrical wall, and opposing side walls having support members that are extendable. The gravity chamber has a first diameter when the support members are contracted, and has a larger second diameter when the support members are extended. The gravity chamber connects to the habitation module with rotating attachment members so that the gravity chamber rotates about an axis. The habitation module also includes an inflatable shell that encompasses the gravity chamber.
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7.发明申请Surface optical reflector, for a space craft such as a geostationary satellite 有权表面光学反射器，用于诸如地球静止卫星的太空飞船公开(公告)号：US20050001101A1
公开(公告)日：2005-01-06
申请号：US10491633
申请日：2002-09-30
申请人： Gilles Maurel
发明人： Gilles Maurel
摘要： Optical surface reflector, for a spacecraft such as a geostationary satellite. The exterior surface (10) of the reflector comprises a plurality of facets (14) inclined to each other and to the interior surface (12) of the reflector. The facets (14) advantageously form a pyramid with a square base in which the angle at the apex is equal to 90°. However, other arrangements are possible without departing from the scope of the invention. The invention increases radiative capacity without significantly increasing mass and overall size.
摘要翻译： 光学表面反射器，用于诸如对地静止卫星的航天器。 反射器的外表面（10）包括彼此倾斜并且与反射器的内表面（12）倾斜的多个小面（14）。 小平面（14）有利地形成具有方形基部的金字塔，其中顶点处的角度等于90°。 然而，在不脱离本发明的范围的情况下，可以进行其它的设置。 本发明增加辐射能力而不显着增加质量和总体尺寸。
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公开(公告)号：US5302130A
公开(公告)日：1994-04-12
申请号：US909293
申请日：1992-07-06
申请人： David L. Sieving
发明人： David L. Sieving
CPC分类号： B64G1/46
摘要： A facility for conditioning people for transition between different gravitational environments. The facility comprises a static cylindrical vessel and a revolving cylindrical habitat within the vessel. Within the revolving habitat are supported a number of habitation levels formed or derived from concave-up circular paraboloids, each shaped and sized so as to produce local net acceleration vectors orthogonal to its upper surface. On any one such surface, the local net acceleration magnitudes within a certain band of radii from the axis of revolution of the habitat will approximate that of the native acceleration present in a particular environment, such as Mars or the Earth. Living areas may be constructed on these surfaces, particularly within the target zones. Access to the habitation levels is provided by a central elevator shaft and system. The habitat is supported hydraulically and caused to revolve by hydromechanical swirling applied at its bottom surface. The preferred embodiments are designed for installation either on or below the surface of a planetary body.
摘要翻译： 调节人们在不同引力环境之间过渡的设施。 该设施包括静态圆柱形容器和容器内的旋转圆柱形栖息地。 在旋转栖息地内支持了一些由凹入圆形抛物面形成或衍生的居住水平，每个形状和大小，以便产生与其上表面正交的局部净加速矢量。 在任何一个这样的表面上，来自栖息地旋转轴的某一半径范围内的局部净加速度大小将接近特定环境中存在的本地加速度，例如火星或地球。 生活区域可以在这些表面上，特别是在目标区域内构建。 中央电梯井和系统提供居住水平。 栖息地由液压支撑，并由其底部施加的液压机械旋转引起旋转。 优选实施例被设计用于安装在行星体的表面上或下方。
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公开(公告)号：US5269482A
公开(公告)日：1993-12-14
申请号：US767794
申请日：1991-09-30
申请人： Ernest J. Shearing
发明人： Ernest J. Shearing
摘要： The protective enclosure for a space vehicle with a magnetic propulsion system includes an insulated Dewar vessel formed of walls of superconducting material surrounded and suspended by superconducting magnets. The superconducting walls shield the interior of the enclosure from external magnetic and electric fields, and the superconducting walls and corresponding magnetics act to cushion passengers or equipment within the enclosure from acceleration or gravitational forces. One or more accelerometers are preferably provided for sensing acceleration or gravity in each of the three orthogonal axes of the enclosure, and a control unit is also preferably provided for controlling the superconducting magnets of the enclosure responsive to output signals from the accelerometers.
摘要翻译： 具有磁力推进系统的空间车辆的保护外壳包括由超导磁体围绕和悬挂的超导材料的壁形成的绝缘杜瓦容器。 超导壁将外壳的内部屏蔽外部磁场和电场，并且超导壁和相应的磁力作用以缓冲外壳内的乘客或设备的加速或重力。 优选地提供一个或多个加速度计用于感测壳体的三个正交轴中的每一个中的加速度或重力，并且还优选地设置控制单元以响应于来自加速度计的输出信号来控制外壳的超导磁体。
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公开(公告)号：US5241836A
公开(公告)日：1993-09-07
申请号：US8427
申请日：1993-01-25
申请人： Vincent T. Bly
发明人： Vincent T. Bly
CPC分类号： B64G1/46 , F24J2/06 , F25B23/003 , Y02E10/44 , Y10S165/904
摘要： A unique structure for constructing the emissive patch of a spaceborne radiative cooler is shown. The structure has very high emissivity for all angles up to a designed-in maximum angle and near zero emissivity for greater angles. The structure also allows the use of high emissivity, nonconducting paints while fully complying with the NASA Electrostatic Discharge Susceptibility requirements for spacecraft. To accomplish these tasks, two previous disadvantages of prior art methods are addressed; eliminating background thermal radiation sources and problems concerning the high emissivity paints used in association with the black body radiator. A reflector consisting of an array of parabolic concentrators is separated from a black body element by an electrically conductive spacer. The concentrators serve to limit the field of view while the conductive spacer eliminates the need to use a conductive paint on the emissive element.
摘要翻译： 示出了用于构建空间辐射冷却器的发射贴片的独特结构。 对于更大的角度，该结构对于所有角度具有非常高的发射率，直到设计的最大角度和接近零的发射率。 该结构还允许使用高发射率，不导电的涂料，同时完全符合NASA静电放电对航天器的敏感性要求。 为了完成这些任务，解决了现有技术方法的两个以前的缺点; 消除背景热辐射源和与黑体散热器相关联使用的高发射率涂料的问题。 由抛物面聚光器阵列组成的反射体通过导电间隔物与黑体元件分离。 集中器用于限制视野，而导电间隔物消除了在发射元件上使用导电涂料的需要。
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