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1. 发明授权

US5390891A Apparatus for mounting equipment in a shock absorbing manner 失效
标题翻译：用于以减震方式安装设备的装置
公开(公告)号：US5390891A
公开(公告)日：1995-02-21
申请号：US72144
申请日：1993-06-04
申请人： Ernst Hornung , Hans Maager , Huba Oery
发明人： Ernst Hornung , Hans Maager , Huba Oery
IPC分类号： B64G5/00 , B64G1/38 , B64G1/64 , B65D81/02 , F16F7/00 , F16F15/00 , F16F15/02 , F16F15/04 , F16F15/06 , F16F15/073 , F16M13/00
CPC分类号： F16F15/04 , F16F15/02 , F16F15/073 , F16F2224/0241
摘要： Shock sensitive equipment, for example, instruments in a spacecraft, must be protected against impacts, for example, those caused by severing explosions that separate the spacecraft from a used up rocket. For this purpose a platform carrying the component to be protected is secured to support structures of the craft by elastic spring devices, each of which has a low eigenfrequency or resonant frequency and a low damping constant, whereby the mounting is preferably so that friction forces are minimized. For example, the spring devices have a U-configuration connected to an L-configuration. Contact surface area minimizing ring spacers may be inserted between the platform and the spring devices.
摘要翻译：冲击敏感设备，例如航天器中的仪器，必须受到保护，防止撞击，例如由将分离飞船与用过的火箭分开的爆炸造成的冲击。为此目的，承载待保护部件的平台通过弹性弹簧装置固定在飞行器的支撑结构上，弹簧装置的本征频率或谐振频率低，阻尼常数低，因此安装优选为使摩擦力为最小化。例如，弹簧装置具有连接到L形构造的U形构造。可以在平台和弹簧装置之间插入最小化环形间隔件的接触表面积。

2. 发明授权

US5271454A Method and apparatus for removing heat generated in a spacecraft 失效
标题翻译：用于去除在航天器中产生的热量的方法和装置
公开(公告)号：US5271454A
公开(公告)日：1993-12-21
申请号：US940505
申请日：1992-09-04
申请人： Bernhard Leidinger
发明人： Bernhard Leidinger
IPC分类号： B64G1/50 , F28D7/02 , F28D7/08 , F25D7/00
CPC分类号： B64G1/50 , Y10S165/911
摘要： Heat is removed from a spacecraft under zero gravity and under various accelerations, by a heat exchange contact between a cooling liquid or coolant and an evaporant or medium to be evaporated. The coolant flowing in at least one liquid cooling circulation circuit and the evaporant which is discharged in its vapor phase, are brought into heat exchange contact with each other in processing chambers forming at least two separate heat exchange stages, wherein different pressure and temperature conditions are set. The cooling liquid or coolant and the medium to be evaporated evaporant flow through these stages in sequence and in such a way that the coolant first flows through the stage with the highest pressure and the highest temperature, and then flows through the stages with successively lower pressure and/or temperature.
摘要翻译：通过冷却液体或冷却剂与要蒸发的蒸发剂或介质之间的热交换接触，在零重力和各种加速度下，从航天器中除去热量。在至少一个液体冷却循环回路中流动的冷却剂和以其气相排出的蒸发器在形成至少两个单独的热交换阶段的处理室中彼此进行热交换接触，其中不同的压力和温度条件是组。冷却液体或冷却剂和待蒸发的介质蒸发器按顺序流过这些阶段，并且使得冷却剂首先以最高压力和最高温度流过级，然后以相继较低的压力流过级和/或温度。

3. 发明授权

US5098040A Micro-g neutral platform for space travel missions 失效
标题翻译：用于空间旅行任务的MICRO-G中性平台
公开(公告)号：US5098040A
公开(公告)日：1992-03-24
申请号：US489459
申请日：1990-03-06
申请人： Ingo Retat
发明人： Ingo Retat
IPC分类号： A63B21/00 , A63B23/00 , B64G1/60 , B64G7/00
CPC分类号： A63B71/0054 , B64G1/60 , A63B2071/0063
摘要： In a device for the support of a vibration exciting apparatus in a spacecraft subjected to gas pressure under weightlessness or microgravitational conditions, especially an apparatus for physical training of a astronaut, a platform for the fastening of the apparatus is provided. For elimination of possible effects upon micro-g sensitive experiments, the platform's position or attitude in the spacecraft can be positioned so that the spacecraft is decoupled from disturbances. For the attitude control, either an aerodynamic stabilization or an actively regulatable linear structural connection with spring and damper effects is provided wherein the energy for the attitude control is produced from the conversion of mechanical energy of the vibration generating apparatus or the training activity of the astronaut.
摘要翻译：在用于支撑在失重或微重力条件下经受气体压力的航天器中的振动激励装置的装置中，特别是用于宇航员体力训练的装置，提供了用于紧固装置的平台。为了消除对微观敏感实验的可能影响，平台在航天器中的位置或姿态可以被定位，使得航天器与扰动分离。对于姿态控制，提供空气动力学稳定或具有弹簧和阻尼器效应的可主动调节的线性结构连接，其中用于姿态控制的能量由振动产生装置的机械能的转换或宇航员的训练活动产生。

4. 发明授权

US4993974A Electrical connector element for orbital stations 失效
标题翻译：用于轨道站的电气连接器元件
公开(公告)号：US4993974A
公开(公告)日：1991-02-19
申请号：US516208
申请日：1990-04-30
申请人： Manfred Baune
发明人： Manfred Baune
IPC分类号： B64G99/00 , H01R24/38 , H01R31/06
CPC分类号： H01R31/06 , B64G9/00 , H01R23/26
摘要： A junction system serves for establishing an electrically conductive connection between a wiring system arranged at a first outer structure and a wiring system arranged at a second inner structure. The respective end regions of the wiring system which have to be interconnected constitute annular receptacles arranged coaxially in tandem, into which a prismatic connector element can be inserted from the outside which comprises on its outer side appropriately designed contact units extending in its longitudinal direction. The quantity of the contact units amounts to a whole or integral multiple of the quantity of the contact pairs to be connected, and these contact units are arranged at the junction element to be offset with respect to each other by a fixed rotational angle.
摘要翻译：接合系统用于在布置在第一外部结构的布线系统和布置在第二内部结构的布线系统之间建立导电连接。必须互连的布线系统的各个端部区域构成串联同轴的环形插座，棱柱形连接器元件可以从外部插入其中，其外侧包括沿其纵向方向延伸的适当设计的接触单元。接触单元的量相当于要连接的接触对数量的整体或整数倍，并且这些接触单元布置在接合元件处以相对于彼此以固定的旋转角度偏移。

5. 发明授权

US4710359A Gas generator 失效
标题翻译：气体发生器
公开(公告)号：US4710359A
公开(公告)日：1987-12-01
申请号：US709510
申请日：1985-03-08
申请人： Hermann Erdmann , Heiko Rahm
发明人： Hermann Erdmann , Heiko Rahm
IPC分类号： B01J7/02 , B64G1/48 , B01J7/00 , B01D13/00 , B01D53/36
CPC分类号： B01J7/02 , B64G1/48
摘要： A gas generator system particularly for use in satellite and orbiting space station is suggested wherein two separate process chambers are alternatingly fed with hydrazine, each chamber includes one or more gas generators proper for catalytically decomposing hydrazine into nitrogen and hydrogen, and further including, and further including two separators for separating the hydrogen from the blend and an interposed supplemental catalytic converter, the two process chambers are interconnected by an intermediate collector type chamber receiving alternatingly nitrogen enriched gas from the two process chambers, and establishing final and complete separation of hydrogen from nitrogen. Hydrogen is extracted from all three chambers; nitrogen is extracted from the intermediate connecting chamber only. The generated gas pressure can be used as energy source for driving the system.
摘要翻译：建议特别用于卫星和轨道空间站的气体发生器系统，其中两个单独的处理室交替地供应肼，每个室包括适合于将肼催化分解成氮和氢的一个或多个气体发生器，并且还包括和进一步包括用于从共混物中分离氢气的两个分离器和一个插入的补充催化转化器，两个处理室通过中间收集器型腔室相互连接，该中间收集器室从两个处理室接收交替的富氮气体，并且从氮气中建立最终和完全的氢气分离。从所有三个室抽取氢气; 仅从中间连接室提取氮气。产生的气体压力可以用作驱动系统的能量源。

6. 发明授权

US4182257A Rescue equipment for submarine crafts 失效
标题翻译：潜艇工艺救援设备
公开(公告)号：US4182257A
公开(公告)日：1980-01-08
申请号：US917080
申请日：1978-06-19
申请人： Eckhard Rolf
发明人： Eckhard Rolf
IPC分类号： B01J7/00 , B63C7/12 , B63C9/18 , B63G8/22 , B63G8/24 , B63G8/40 , B63C7/00
CPC分类号： B63G8/40 , B63G8/22 , B63G8/24
摘要： An auxiliary gas source for blowing a ballast tank of a submarine craft includes a casing with a store for pressure gas, a container for liquid and a gas generator proper into which the liquid can be forced by the gas. The liquid is contained in a flexible bag and the pressure gas acts on the bag from the outside, to be separately discharged as a supplemental supply of gas.
摘要翻译：用于吹制海底艇的压载舱的辅助气源包括：具有压力气体储存器的壳体，用于液体的容器和气体发生器，液体可被气体压迫。液体被包含在柔性袋中，并且压力气体从外部作用在袋上，作为补充气体分开排出。

7. 发明授权

US3754439A Oceanological and meteorological station 失效
标题翻译：海洋与气象台
公开(公告)号：US3754439A
公开(公告)日：1973-08-28
申请号：US3754439D
申请日：1971-08-02
申请人： ERNO RAUMFAHRTTECHNIK GMBH
发明人： BAUER P
IPC分类号： B63B22/04 , G01V9/00 , G01W1/00
CPC分类号： B63B22/04
摘要： Equipment establishing a station for providing for oceanological and meteorological measurements in the continental shelf region and in similar, shallow parts of the ocean, and having a base anchoring the station to the bottom of the ocean, a mast pivotally linked to the base for up and down pivoting as well as for turning on a vertical axis; and variable buoyancy is provided at the mast above the point of pivoting. Instrumentation, including sensing means for taking oceanological and meteorological readings as well as a radio receiver transmitter and a controller are disposed on top of the mast.
摘要翻译：在大陆架区域和类似的浅海部分建立一个用于提供海洋和气象测量的台站的设备，以及将站点固定在海底的基座，一个枢轴连接到基座上的桅杆，向下枢转以及垂直轴的转动; 并且在枢转点之上的桅杆处设置可变浮力。包括用于摄取海洋和气象读数的检测装置以及无线电接收器发射器和控制器的仪器被布置在桅杆的顶部。

8. 发明授权

US5485721A Arcjet for a space flying body 失效
标题翻译： Arcjet为空间飞行的身体
公开(公告)号：US5485721A
公开(公告)日：1996-01-23
申请号：US268807
申请日：1994-06-30
申请人： Manfred Steenborg
发明人： Manfred Steenborg
IPC分类号： F02K9/68 , F03H1/00 , H05H1/32 , H05H1/34
CPC分类号： B64G1/406 , F02K9/68 , H05H1/32 , B64G1/24 , H05H2001/3484
摘要： A thermal arcjet propulsion plant is particularly constructed for position and orbit corrections in a space flying body or spacecraft. A housing forms an anode and an expansion nozzle. An elongated rod mounted in an electrically insulating manner centrally in the housing forms the cathode which reaches with its tip into a plenum chamber just upstream of the nozzle. Propellant components formed by dissociating ammonia are injected into the plenum chamber. A small gap is provided between the tip of the cathode and the restrictor of the nozzle. An arc is ignited in this gap and the thermal arc energy is taken up by the by propellant. A dissociation chamber for the by propellant is arranged around the housing. The arrangement is such that the chamber in which the gas dissociation takes place is arranged in series with and upstream of the plenum chamber. The cathode is also arranged in series with the restrictor and the nozzle. The cathode is connected through a flexible electrical conductor to an electric power supply. Similarly, the housing forming the anode is connected to the same power supply. The dissociation chamber includes a catalyst for a catalytic and/or thermal dissociation of the ammonia into its components of hydrogen and nitrogen.
摘要翻译：热电弧喷射推进装置特别构造用于空间飞行体或航天器中的位置和轨道校正。壳体形成阳极和膨胀喷嘴。在壳体中央以电绝缘方式安装的细长杆形成阴极，该阴极通过其尖端进入恰好在喷嘴上游的增压室。通过解离氨形成的推进剂组分被注入增压室。在阴极的尖端和喷嘴的节流器之间设置小的间隙。在该间隙中点燃电弧，并且热电弧能量被推进剂吸收。用于推进剂的解离室布置在壳体周围。这种布置使得其中发生气体解离的室被布置成与增压室串联并且在增压室的上游。阴极还与限流器和喷嘴串联布置。阴极通过柔性电导体连接到电源。类似地，形成阳极的壳体连接到相同的电源。解离室包括用于催化和/或热解离氨到其氢和氮的组分中的催化剂。

9. 发明授权

US5358033A Heat pipe, with a cooled bubble trap 失效
标题翻译：热管，带有冷却的气泡阱
公开(公告)号：US5358033A
公开(公告)日：1994-10-25
申请号：US158422
申请日：1993-11-29
申请人： Reinhard Schlitt
发明人： Reinhard Schlitt
IPC分类号： F28D15/02
CPC分类号： F28D15/0275 , F28D15/0258 , F28F1/16
摘要： A heat pipe structure, especially for cooling in a spacecraft, is equipped with a main heat pipe and at least one smaller diameter auxiliary heat pipe arranged so that the main and auxiliary pipes are in thermal contact with each other at the evaporator end of the main heat pipe. The condenser end of the auxiliary heat pipe, or pipes, is connected in a heat exchange manner with an auxiliary radiator or heat exchanger which is smaller than and thermally insulated from a main heat exchanger, the latter being in thermal contact with the condenser end of the main heat pipe. The auxiliary heat pipe, or pipes, super cools a bubble trap in the main heat pipe for removing of gas and/or vapor bubbles from the liquid flow path of the main heat pipe.
摘要翻译：特别是用于在航天器中冷却的热管结构配备有主热管和至少一个较小直径的辅助热管，其布置成使主管和辅管在主蒸发器端处彼此热接触热管。辅助热管或冷凝器的冷凝器端部与热交换器连接，辅助散热器或热交换器与主热交换器小而热绝缘，后者与主热交换器主热管。辅助热管或管道超级冷却主热管中的气泡阱，用于从主热管的液体流动路径去除气体和/或蒸汽气泡。

10. 发明授权

US5139589A Fuel for use independently of atmospheric air and method for producing the fuel 失效
标题翻译：用于大气环境的燃料和生产燃料的方法
公开(公告)号：US5139589A
公开(公告)日：1992-08-18
申请号：US731543
申请日：1991-07-17
申请人： Joerg Hartmanns
发明人： Joerg Hartmanns
IPC分类号： C06B27/00 , C10L1/00 , C10L1/10 , C10L1/12 , C10L1/16 , C10L1/18
CPC分类号： C06B27/00 , C10L1/00 , C10L1/10 , C10L1/1216 , C10L1/1233 , C10L1/125 , C10L1/1608 , C10L1/188
摘要： A fuel for use independently of atmospheric air by reaction with an oxidizer, has a metal hydride as a solid fuel component mixed into an inert liquid fuel component and 1.5 to 5.0 weight percent of a stearate as part of the solid fuel component. The liquid fuel component is preferably an easy flowing paraffin into which the stearate and the solid fuel component are mixed to form a liquified fuel that will react with a liquid oxidizer. The mixing is preferably performed at a temperature above 100.degree. C. and at a reduced pressure less than 10.sup.5 Pa.
摘要翻译：作为与氧化剂反应的独立于大气的燃料，在固体燃料成分中作为固体燃料成分混入惰性液体燃料成分和1.5〜5.0重量％的硬脂酸盐中。液体燃料组分优选是容易流动的石蜡，其中将硬脂酸盐和固体燃料组分混合以形成将与液体氧化剂反应的液化燃料。混合优选在高于100℃的温度下和小于105Pa的减压下进行。

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