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1. 发明授权

US06439516B1 Support structure having alternative states of high strength or low thermal conductivity, and connecting strut 失效
标题翻译：支撑结构具有高强度或低热导率的替代状态，以及连接支柱
公开(公告)号：US06439516B1
公开(公告)日：2002-08-27
申请号：US09898673
申请日：2001-07-03
申请人： Martin Roth , Franz Sperber , Adalbert Wagner
发明人： Martin Roth , Franz Sperber , Adalbert Wagner
IPC分类号： A47G2302
CPC分类号： B64G1/641 , B64G1/645 , F17C13/088 , Y10S248/901
摘要： A support structure includes at least one shaped component which is produced from a shape memory alloy and which, in a first operating state of the support structure, results in an increase in the strength of the support structure and, in a second operating state, results in a reduction in the thermal conductivity of the support structure. The first strut structure is surrounded by a second strut structure, which has a higher mechanical strength in comparison with the first strut structure, and the first strut structure is connected securely, at least at one of its ends, to the second strut structure. In addition, the first strut structure is connected to a holding device, and the second strut structure is releasably connected to the holding device by the at least one shaped component.
摘要翻译：支撑结构包括由形状记忆合金制成的至少一个成形部件，并且在支撑结构的第一操作状态下导致支撑结构的强度增加，并且在第二操作状态下，结果在支撑结构的热导率的降低。第一支柱结构被第二支柱结构包围，第二支柱结构与第一支柱结构相比具有较高的机械强度，并且第一支柱结构至少在其一端处可靠地连接到第二支柱结构。此外，第一支柱结构连接到保持装置，并且第二支柱结构通过至少一个成形部件可释放地连接到保持装置。

2. 发明申请

US20050016179A1 Extendible exhaust nozzle bell for a rocket engine 有权
标题翻译：可扩展的排气喷嘴钟为火箭发动机
公开(公告)号：US20050016179A1
公开(公告)日：2005-01-27
申请号：US10803899
申请日：2004-03-19
申请人： Martin Roth , Rita Roth , Franz Sperber
发明人： Martin Roth , Rita Roth , Franz Sperber
IPC分类号： F02K9/97 , F02K1/09
CPC分类号： F02K9/976
摘要： An exhaust nozzle bell for a rocket engine including a first part arranged on a motor of the rocket engine, and a second part coupled to the first part. The second part having a stowed position in which the second part surrounds the first part and is positioned closer to the motor, and an operating position in which the first part and the second part form a continuous shape and the second part is arranged farther from the motor. Moreover, the nozzle can include an extension mechanism structured and arranged to extend the second part from the stowed position to the operating position, the extension mechanism including a plurality of swiveling extension arms, wherein the extension arms have first and second ends. Furthermore, each of the extension arms comprise one of a sliding and rolling element on an end facing the second part of the exhaust nozzle bell. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
摘要翻译：一种用于火箭发动机的排气喷嘴钟，包括布置在火箭发动机的马达上的第一部分，以及耦合到第一部分的第二部分。第二部分具有收纳位置，其中第二部分围绕第一部分并且位于更接近电动机的位置;以及操作位置，其中第一部分和第二部分形成连续形状，并且第二部分布置成更远离发动机。此外，喷嘴可以包括延伸机构，其构造和布置成将第二部分从收起位置延伸到操作位置，延伸机构包括多个旋转延伸臂，其中延伸臂具有第一和第二端。此外，每个延伸臂在面向排气喷嘴钟的第二部分的端部上包括滑动和滚动元件中的一个。本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

3. 发明授权

US06555740B2 Extendible solar generator with an extendible supporting array structure 有权
标题翻译：可扩展太阳能发电机具有可扩展的支撑阵列结构
公开(公告)号：US06555740B2
公开(公告)日：2003-04-29
申请号：US09968709
申请日：2001-10-02
申请人： Martin Roth , Franz Sperber , Walter Stich
发明人： Martin Roth , Franz Sperber , Walter Stich
IPC分类号： H01L31045
CPC分类号： B64G1/443 , B64G1/222 , H02S30/20 , Y10S136/291 , Y10S136/292
摘要： An extendible solar generator has an extendible solar cell structure and an extendible support array structure which has a first cross member and is connected with a stowage housing for the solar cell structure. The support array structure can be rolled out independently of the solar cell structure and has guiding devices for rolling out the solar cell structure after the array structure has rolled out.
摘要翻译：可延伸的太阳能发电机具有可延伸的太阳能电池结构和可延伸的支撑阵列结构，其具有第一横向构件并与用于太阳能电池结构的收纳壳体连接。可以独立于太阳能电池结构推出支撑阵列结构，并且在阵列结构已经推出之后具有用于推出太阳能电池结构的引导装置。

4. 发明授权

US06229501B1 Reflector and reflector element for antennas for use in outer space and a method for deploying the reflectors 失效
标题翻译：用于外层空间的天线的反射器和反射器元件以及用于部署反射器的方法
公开(公告)号：US06229501B1
公开(公告)日：2001-05-08
申请号：US09298661
申请日：1999-04-23
申请人： Martin Roth , Franz Sperber
发明人： Martin Roth , Franz Sperber
IPC分类号： H01Q1520
CPC分类号： H01Q1/288 , B64G1/66 , H01Q15/161
摘要： An antenna reflector for satellites or space vehicles having a number of hexagonal individual reflectors (1) which can be arranged around a rigid central element (2). The reflectors (1) are connected to the central element (2) by a support structure (3) that can collapse to hold the reflectors in a compact storage state or be extended to deploy the reflectors. The reflectors (1) are folded like an umbrella in a transport state when the reflectors are collapsed and at the place of use, they are brought into their operating positions and spread out, so that they collectively form a reflector surface. Each reflector (1) has a foldable surface structure connected by a multiple number of ribs (11) to a rigid, central structure (12).
摘要翻译：一种用于卫星或航天器的天线反射器，其具有多个可以布置在刚性中心元件（2）周围的六边形单个反射器（1）。反射器（1）通过支撑结构（3）连接到中心元件（2），支撑结构（3）可以折叠以将反射器保持在紧凑的存储状态，或者延伸以部署反射器。反射器（1）在反射器被折叠时在运输状态下像伞一样折叠，并且在使用的地方，它们进入其操作位置并展开，从而它们共同形成反射器表面。每个反射器（1）具有通过多个肋（11）连接到刚性中心结构（12）的可折叠表面结构。

5. 发明授权

US06201515B1 Method and apparatus for producing an antenna reflector, and a structure for such a reflector 失效
标题翻译：用于制造天线反射器的方法和装置以及这种反射器的结构
公开(公告)号：US06201515B1
公开(公告)日：2001-03-13
申请号：US09298660
申请日：1999-04-23
申请人： Franz Sperber , Martin Roth , Jürgen Dupier
发明人： Franz Sperber , Martin Roth , Jürgen Dupier
IPC分类号： H01Q2112
CPC分类号： H01Q15/141 , H01Q1/08 , H01Q15/161 , Y10T29/49016
摘要： A method for the production of a reflector for antennas to be used in outer space in which a thread (7) is wound on a winding spindle (1), to obtain a netting or network structure. The winding spindle (1) has contour segments (2) on its surface, whose contour corresponds to the contour of a sector of the reflector surface being produced. After winding, the resulting thread network structure is hardened on the winding spindle (1) and the thread network structure is divided into individual sections. The contour segments (2) are separated from the winding spindle (1) and together with the sections of the hardened network structure thereon are fitted together on an assembly rig so that the individual sections collectively form a reflector. The winding of the thread of the network structure on the spindle can vary in at least one direction or in its angle of placement a, so that the network structure has a different, selectable rigidity in individual areas.
摘要翻译：一种用于生产用于外圈的天线的反射器的方法，其中线（7）缠绕在卷绕轴（1）上，以获得网状或网状结构。卷绕轴（1）在其表面上具有轮廓段（2），其轮廓对应于正在产生的反射器表面的扇形轮廓。绕组后，所得螺纹网络结构在卷绕轴（1）上硬化，螺纹网状结构分为单独部分。轮廓段（2）与卷绕轴（1）分离，并且与其上的硬化网络结构的部分一起装配在组装钻机上，使得各个部分共同形成反射器。网络结构在主轴上的线圈的缠绕可以在至少一个方向或其放置角度α上变化，使得网络结构在各个区域中具有不同的可选刚性。

6. 发明申请

US20060276248A1 Mechanical rotational drive 有权
公开(公告)号：US20060276248A1
公开(公告)日：2006-12-07
申请号：US11429943
申请日：2006-05-09
申请人： Franz Sperber , Walter Stich , Leonhard Stielner , Adalbert Wagner
发明人： Franz Sperber , Walter Stich , Leonhard Stielner , Adalbert Wagner
IPC分类号： F16D3/00
CPC分类号： F16F15/063 , B64G1/222 , F16F1/16
摘要： A mechanical rotational drive has a bar-like torsion element, whereby the torsion element is firmly clamped with a first end in a bearing device. The torsion element can be pivoted with a second free end with respect to the clamped end about the longitudinal axis, forming a rotation axis, of the torsion element between a relaxed position and a tensioned position, whereby the length of the torsion element is reduced with respect to the relaxed position when the torsion element is brought into its tensioned position. A device for transmitting a torque into the torsion element or out of the torsion element is provided in the area of the free end, and a damping device is arranged in the axial direction of the torsion element at a fixed distance from the bearing device and adjacent to the free end of the torsion element, and a damping part is provided on the torsion element in the area of the free end of the torsion element, which damping part in the relaxed position is in friction engagement with the damping device and which in the tensioned position is not engaged with the damping device.

7. 发明授权

US4589679A Safety steering column made of fiber-reinforced synthetic materials 失效
标题翻译：由纤维增强合成材料制成的安全转向柱
公开(公告)号：US4589679A
公开(公告)日：1986-05-20
申请号：US615347
申请日：1984-05-30
申请人： Peter Wackerle , Ralf-Thilo Schulz , Franz Sperber , Wolfram Koletzko , Wolfgang Prochaska
发明人： Peter Wackerle , Ralf-Thilo Schulz , Franz Sperber , Wolfram Koletzko , Wolfgang Prochaska
IPC分类号： B32B5/00 , B29C53/58 , B29C70/20 , B32B1/08 , B62D1/18 , B62D1/19 , F16C3/02
CPC分类号： B62D1/192 , B29C70/207 , B29C53/58
摘要： A safety steering column made of wound fiber-reinforced synthetic materials manufactured economically and simply, yet simultaneously with due regard to its deformation characteristics in response to axial compressive overloading under various operating conditions. For this purpose the steering column is wound as a rotationally symmetrical tubular body having five component integral sections (3, 4, 5, 6, and 7). The component sections (3 and 7) are relatively thick-walled connecting tubes to provide a torque input section and a torque output section provided with connectors (8) for steering wheel hub and for a steering mechanism. An intermediate section (5) of the steering column is a cylindrical, relatively thin-walled tube with a larger diameter (d.sub.2) compared to the connecting sections. Conical transition sections (4 and 6) preferably extend between the intermediate section and the connecting tubes or sections. The wall thickness of these transition sections diminishes uniformly from the connecting section in the direction toward the intermediate section for improving the buckling ability. A geodetic winding procedure is preferably applied for winding the columns.
摘要翻译：由缠绕的纤维增强合成材料制成的安全转向柱经济地和简单地制造，同时适当地考虑到其在各种操作条件下的轴向压缩过载的变形特性。为此，转向柱被卷绕成具有五个部件积分部分（3,4,5,6和7）的旋转对称管状体。部件部分（3和7）是相对厚壁的连接管，以提供转矩输入部分和设置有用于方向盘轮毂和转向机构的连接器（8）的扭矩输出部分。转向柱的中间部分（5）是与连接部分相比具有较大直径（d2）的圆柱形相对薄壁的管。锥形过渡部分（4和6）优选地在中间部分和连接管或部分之间延伸。这些过渡部分的壁厚在朝向中间部分的方向上从连接部分均匀地减小，以提高屈曲能力。优选地应用大地测量卷绕程序以卷绕柱。

8. 发明授权

US5042395A Composite vehicle body having sandwich panels integrally formed with frame parts to form individual body modules which are connected to other body modules to form the vehicle body 失效
标题翻译：复合车体具有与框架部件一体形成的夹层板，以形成连接到其他主体模块以形成车体的单独主体模块
公开(公告)号：US5042395A
公开(公告)日：1991-08-27
申请号：US434272
申请日：1989-11-13
申请人： Peter M. Wackerle , Franz Sperber , Josef Grober
发明人： Peter M. Wackerle , Franz Sperber , Josef Grober
IPC分类号： B61D17/00 , B61D17/04 , B62D31/02
CPC分类号： B61D17/045 , B61D17/00
摘要： A rail vehicle body consisting of a support frame and sandwich parts attached thereto having an outer and an inner cover layer and supporting layer glued in between them, comprises, with a view to cost-effective fabrication and above all reduction of assembly cost, individually made body modules which are designed in integral construction as a sandwich structure with support frame parts inserted in the region of the supporting layer and fastened to the cover layers and being provided at the edges of the support frame parts with fitting connections for assembly of the body modules.
摘要翻译：由支撑框架和附接到其上的夹层部件组成的轨道车身主体具有外侧和内侧覆盖层以及胶合在它们之间的支撑层，其特征在于，为了具有成本有效的制造和首先降低组装成本，单独制造主体模块设计成整体构造为夹层结构，支撑框架部分插入支撑层的区域并且紧固到覆盖层并且设置在支撑框架部分的边缘处，具有用于组装主体模块的装配连接。

9. 发明授权

US4732542A Large airfoil structure and method for its manufacture 失效
标题翻译：大型翼型结构及其制造方法
公开(公告)号：US4732542A
公开(公告)日：1988-03-22
申请号：US885239
申请日：1986-07-14
申请人： Michael Hahn , Franz Sperber
发明人： Michael Hahn , Franz Sperber
IPC分类号： B32B5/18 , B64C3/18 , B64C27/473 , F03D1/06 , F03D11/00 , B64C11/26
CPC分类号： B64C27/473 , F03D1/065 , B64C2027/4736 , F05B2240/30 , Y02E10/721 , Y02P70/523
摘要： An airfoil particularly suited for use in rotor blades of large wind-drivenower plants is formed in three modular sections including a nose or leading section, a spar section and a trailing section, each separately formed and subsequently assembled. In the method of the invention the spar section is formed in two separate mold units which are configured to form part of the upper and lower aerodynamic profile of the airfoil and the two spar section units are trimmed along a junction plane and then joined together at the junction plane to form the spar section of the airfoil.
摘要翻译：特别适合用于大型风力发电厂的转子叶片的翼型件形成在三个模块部分中，包括鼻部或前部，翼梁部分和尾部部分，每个单独形成并随后组装。在本发明的方法中，翼梁部分形成在两个单独的模具单元中，其被构造成形成翼型的上部和下部空气动力学轮廓的一部分，并且两个翼梁段单元沿着接合平面修剪，然后在连接平面以形成翼型的翼梁部分。

10. 发明授权

US5365828A Pneumatic linear drive comprising a locking mechanism for end positions 失效
标题翻译：气动线性驱动器，包括用于端部位置的锁定机构
公开(公告)号：US5365828A
公开(公告)日：1994-11-22
申请号：US79907
申请日：1993-06-23
申请人： Franz Sperber , Arno Voit , Walter Stich
发明人： Franz Sperber , Arno Voit , Walter Stich
IPC分类号： F15B15/26
CPC分类号： F15B15/261
摘要： A linear drive is disclosed comprising a single-acting pneumatic piston cylinder unit, at least one spring which acts against the pneumatic force and loads the piston rod in the direction of one end position, and one form-locking pneumatic locking mechanism respectively for each of the two end positions of the piston rod. The locking mechanism comprises a locking link which can be locked from diametrical sides into one recess of the piston rod respectively; a first control piston which is rigidly connected with the locking link, a second larger control piston which is disposed in a longitudinally movable manner on a supporting tube rigidly connected with the locking link; a spring which presses the second control piston in the direction of its extreme end position; a stop for the second control piston which is fixed to the housing; a valve piston which is coupled in a springy and sealing manner with the second control piston and has a closable throttle duct and an open flow connection from the interior of the second control piston and of the valve piston to the pressure space of the piston cylinder unit.
摘要翻译：公开了一种线性驱动器，其包括单作用气动活塞气缸单元，至少一个弹簧，其抵抗气动力并且沿一端位置的方向负载活塞杆，以及一个形成锁定气动锁定机构，活塞杆的两端位置。锁定机构包括一个可以从直径侧锁定到活塞杆的一个凹槽中的锁定连杆; 第一控制活塞，其与所述锁定连杆刚性地连接;第二较大的控制活塞，其以纵向移动的方式设置在与所述锁定连杆刚性连接的支撑管上; 弹簧，其沿着其最终位置的方向按压第二控制活塞; 用于固定到壳体的第二控制活塞的止动件; 阀活塞以弹性和密封方式与第二控制活塞联接，并且具有可从第二控制活塞和阀活塞的内部到活塞气缸单元的压力空间的可关闭节气门管道和开放流动连接。

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