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1. 发明授权

US07192229B2 Apparatus for releasably securing a load to a structure 有权
标题翻译：用于将负载可释放地固定到结构的装置
公开(公告)号：US07192229B2
公开(公告)日：2007-03-20
申请号：US11099219
申请日：2005-04-04
申请人： Ingo Retat , Guenter Boerchers , Volker Groth , Wolfgang Tritsch
发明人： Ingo Retat , Guenter Boerchers , Volker Groth , Wolfgang Tritsch
IPC分类号： B60P1/64
CPC分类号： B64G1/222 , B64G1/645
摘要： A load, such as a pallet, is releasably secured to a fixed structure, e.g. a cargo bay of a space shuttle. The pallet (5) is secured to a support (2), which holds the pallet and is secured in the cargo bay. A first interlocking device (ID1) is provided at each end of the support. A second interlocking device (ID2) is provided at each end of the pallet. The first interlocking device (ID1) includes a shaft (1) rotatably held in a shaft mounting bracket (3A) secured to a respective support end (3). The second interlocking device (ID2) includes a bracket (4) secured to an end of the pallet (5), a claw (4A) secured to the bracket, a groove in the claw (4A) and a fork (6) in the groove of the claw (4A). A central shaft section (1A) is received in the fork (6) for the interlocking. The shaft (1) is movable in the fork (6) in the direction of the x-axis and of the z-axis. The shaft is also rotatable about the x-axis and tiltable relative to the y-axis. The fork is turnable about the z-axis. These motions are possible in the locked state due to the construction of the interlocking devices (ID1 and ID2). In the unlocked state, jamming and even seizing are avoided or minimized by increasing play.
摘要翻译：负载，例如托盘，可释放地固定到固定结构，例如，航天飞机的货舱。托盘（5）固定到支撑件（2）上，托架（2）固定托盘并固定在货舱中。第一联锁装置（ID 1）设置在支撑件的每一端。在托盘的每一端设有第二联锁装置（ID 2）。第一联锁装置（ID 1）包括可旋转地保持在固定到相应的支撑端（3）上的轴安装支架（3A）中的轴（1）。第二联锁装置（ID2）包括固定到托盘（5）的端部的支架（4），固定到支架的爪（4A），爪（4A）中的槽和叉（6））在爪（4A）的凹槽中。中心轴部分（1A）被容纳在叉（6）中用于互锁。轴（1）可以在叉（6）中沿x轴和z轴的方向移动。轴也可围绕x轴旋转并相对于y轴可倾斜。叉可绕z轴转动。由于联锁装置（ID 1和ID 2）的结构，这些运动在锁定状态下是可能的。在解锁状态下，通过增加播放来避免或最小化卡住，甚至卡住。

2. 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。

3. 发明申请

US20060088366A1 Non-explosive device for releasably securing components 有权
标题翻译：用于可拆卸地固定部件的非爆炸装置
公开(公告)号：US20060088366A1
公开(公告)日：2006-04-27
申请号：US11174436
申请日：2005-07-01
申请人： Ingo Retat , Barbara Klotz , Jens Wendorff , Oliver Hoeni
发明人： Ingo Retat , Barbara Klotz , Jens Wendorff , Oliver Hoeni
IPC分类号： F01D5/02
CPC分类号： B64G1/645 , B64G1/222 , B64G1/641 , Y10T403/11 , Y10T403/16 , Y10T403/1641 , Y10T403/21
摘要： An arrangement for releasably securing or connecting together at least two components includes a securing element that interconnects the components and that can be melted, thermally decomposed or otherwise separated by applying heat thereto. The securing element is preferably a monofilament or multifilament thread of natural or synthetic material, such as high strength polymer material. The arrangement further preferably includes a compression bracing structure such as a housing that bears compression forces between the components, while the securing element bears tension forces. The arrangement further preferably includes an electric resistance heating element that can be electrically energized and is arranged to apply heat to the thread, so as to melt or decompose and separate the thread and thereby release and separate the two interconnected components.
摘要翻译：用于将至少两个部件可释放地固定或连接在一起的装置包括固定元件，其将部件互连，并且可通过向其施加热而熔化，热分解或以其它方式分离。固定元件优选是天然或合成材料的单丝或多丝线，例如高强度聚合物材料。该装置还优选地包括压缩支撑结构，例如在组件之间承受压缩力的壳体，同时固定元件承受张力。该装置还优选地包括电阻加热元件，该电阻加热元件可被电激励并且被布置成对螺纹施加热量，以便熔化或分解和分离螺纹，从而释放和分离两个相互连接的部件。

4. 发明申请

US20050232745A1 Apparatus for releasably securing a load to a structure 有权
标题翻译：用于将负载可释放地固定到结构的装置
公开(公告)号：US20050232745A1
公开(公告)日：2005-10-20
申请号：US11099219
申请日：2005-04-04
申请人： Ingo Retat , Guenter Boerchers , Volker Groth , Wolfgang Tritsch
发明人： Ingo Retat , Guenter Boerchers , Volker Groth , Wolfgang Tritsch
IPC分类号： B64G1/22 , B64G1/64 , B65G1/133
CPC分类号： B64G1/222 , B64G1/645
摘要： A load, such as a pallet, is releasably secured to a fixed structure, e.g. a cargo bay of a space shuttle. The pallet (5) is secured to a support (2), which holds the pallet and is secured in the cargo bay. A first interlocking device (ID1) is provided at each end of the support. A second interlocking device (ID2) is provided at each end of the pallet. The first interlocking device (ID1) includes a shaft (1) rotatably held in a shaft mounting bracket (3A) secured to a respective support end (3). The second interlocking device (ID2) includes a bracket (4) secured to an end of the pallet (5), a claw (4A) secured to the bracket, a groove in the claw (4A) and a fork (6) in the groove of the claw (4A). A central shaft section (1A) is received in the fork (6) for the interlocking. The shaft (1) is movable in the fork (6) in the direction of the x-axis and of the z-axis. The shaft is also rotatable about the x-axis and tiltable relative to the y-axis. The fork is turnable about the z-axis. These motions are possible in the locked state due to the construction of the interlocking devices (ID1 and ID2). In the unlocked state, jamming and even seizing are avoided or minimized by increasing play.
摘要翻译：负载，例如托盘，可释放地固定到固定结构，例如，航天飞机的货舱。托盘（5）固定到支撑件（2）上，托架（2）固定托盘并固定在货舱中。第一联锁装置（ID 1）设置在支撑件的每一端。在托盘的每一端设有第二联锁装置（ID 2）。第一联锁装置（ID 1）包括可旋转地保持在固定到相应的支撑端（3）上的轴安装支架（3A）中的轴（1）。第二联锁装置（ID2）包括固定到托盘（5）的端部的支架（4），固定到支架的爪（4A），爪（4A）中的槽和叉（6））在爪（4A）的凹槽中。中心轴部分（1A）被容纳在叉（6）中用于互锁。轴（1）可以在叉（6）中沿x轴和z轴的方向移动。轴也可围绕x轴旋转并相对于y轴可倾斜。叉可绕z轴转动。由于联锁装置（ID 1和ID 2）的结构，这些运动在锁定状态下是可能的。在解锁状态下，通过增加播放来避免或最小化卡住，甚至卡住。

5. 发明授权

US08302748B2 Multi-axis spring damping system for a payload in a spacecraft 有权
标题翻译：用于航天器有效载荷的多轴弹簧阻尼系统
公开(公告)号：US08302748B2
公开(公告)日：2012-11-06
申请号：US12387868
申请日：2009-05-07
申请人： Ingo Retat , Kiyoumars Abdoly , Horst Koehler , Wolfgang Tritsch
发明人： Ingo Retat , Kiyoumars Abdoly , Horst Koehler , Wolfgang Tritsch
IPC分类号： F16F7/10
CPC分类号： F16F15/046 , B64G1/14 , B64G1/641 , F16F2228/08
摘要： A multi-axis spring damping element includes two spring damping cushion members received between caps on a bolt shaft, and an axial adjustment mechanism at a free end of the bolt shaft. The other end of the bolt shaft is connected to a support structure, and a load to be supported in a vibration-damped manner is carried by intermediate caps between the two spring damping cushion members. A plurality of such spring damping elements forms a spring damping system, for example for supporting a payload-carrying pallet on a load platform of a spacecraft.
摘要翻译：多轴弹簧阻尼元件包括容纳在螺栓轴上的盖之间的两个弹簧阻尼缓冲件和在螺栓轴的自由端的轴向调节机构。螺栓轴的另一端连接到支撑结构，并且以两个弹簧阻尼缓冲构件之间的中间盖承载以振动阻尼的方式支撑的负载。多个这样的弹簧阻尼元件形成弹簧阻尼系统，例如用于在载具平台上支撑载货物托盘。

6. 发明申请

US20090278292A1 Multi-axis spring damping system for a payload in a spacecraft 有权
标题翻译：用于航天器有效载荷的多轴弹簧阻尼系统
公开(公告)号：US20090278292A1
公开(公告)日：2009-11-12
申请号：US12387868
申请日：2009-05-07
申请人： Ingo Retat , Kiyoumars Abdoly , Horst Koehler , Wolfgang Tritsch
发明人： Ingo Retat , Kiyoumars Abdoly , Horst Koehler , Wolfgang Tritsch
IPC分类号： F16F15/04
CPC分类号： F16F15/046 , B64G1/14 , B64G1/641 , F16F2228/08
摘要： A multi-axis spring damping element includes two spring damping cushion members received between caps on a bolt shaft, and an axial adjustment mechanism at a free end of the bolt shaft. The other end of the bolt shaft is connected to a support structure, and a load to be supported in a vibration-damped manner is carried by intermediate caps between the two spring damping cushion members. A plurality of such spring damping elements forms a spring damping system, for example for supporting a payload-carrying pallet on a load platform of a spacecraft.
摘要翻译：多轴弹簧阻尼元件包括容纳在螺栓轴上的盖之间的两个弹簧阻尼缓冲件和在螺栓轴的自由端的轴向调节机构。螺栓轴的另一端连接到支撑结构，并且以两个弹簧阻尼缓冲构件之间的中间盖承载以振动阻尼的方式支撑的负载。多个这样的弹簧阻尼元件形成弹簧阻尼系统，例如用于在载具平台上支撑载货物托盘。

7. 发明授权

US07396182B2 Non-explosive device for releasably securing components 有权
标题翻译：用于可拆卸地固定部件的非爆炸装置
公开(公告)号：US07396182B2
公开(公告)日：2008-07-08
申请号：US11174436
申请日：2005-07-01
申请人： Ingo Retat , Barbara Klotz , Jens Wendorff , Oliver Hoeni
发明人： Ingo Retat , Barbara Klotz , Jens Wendorff , Oliver Hoeni
IPC分类号： H01H71/20
CPC分类号： B64G1/645 , B64G1/222 , B64G1/641 , Y10T403/11 , Y10T403/16 , Y10T403/1641 , Y10T403/21
摘要： An arrangement for releasably securing or connecting together at least two components includes a securing element that interconnects the components and that can be melted, thermally decomposed or otherwise separated by applying heat thereto. The securing element is preferably a monofilament or multifilament thread of natural or synthetic material, such as high strength polymer material. The arrangement further preferably includes a compression bracing structure such as a housing that bears compression forces between the components, while the securing element bears tension forces. The arrangement further preferably includes an electric resistance heating element that can be electrically energized and is arranged to apply heat to the thread, so as to melt or decompose and separate the thread and thereby release and separate the two interconnected components.
摘要翻译：用于将至少两个部件可释放地固定或连接在一起的装置包括固定元件，其将部件互连，并且可通过向其施加热而熔化，热分解或以其它方式分离。固定元件优选是天然或合成材料的单丝或多丝线，例如高强度聚合物材料。该装置还优选地包括压缩支撑结构，例如在组件之间承受压缩力的壳体，同时固定元件承受张力。该装置还优选地包括电阻加热元件，该电阻加热元件可被电激励并且被布置成对螺纹施加热量，以便熔化或分解和分离螺纹，从而释放和分离两个相互连接的部件。

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