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1. 发明授权

US06276639B1 Apparatus for launching and deploying multiple satellites 有权
标题翻译：发射和部署多颗卫星的装置
公开(公告)号：US06276639B1
公开(公告)日：2001-08-21
申请号：US09458492
申请日：1999-12-09
申请人： Ernst Hornung , Huba Ory , Andreas Rittweger , Markus Quadt , Peter Borgwardt , Joerg Bolz
发明人： Ernst Hornung , Huba Ory , Andreas Rittweger , Markus Quadt , Peter Borgwardt , Joerg Bolz
IPC分类号： B64G100
CPC分类号： B64G1/002 , B64G1/1085 , B64G1/641 , B64G1/645 , B64G2001/643
摘要： An apparatus for launching and dispensing multiple satellites into orbit includes a central structure and a plurality of satellites releasably bundled around the central structure to form a cohesive, single payload mounted on an upper stage of a launcher rocket. The central structure includes a central tube and an adapter shell that fits onto the upper stage of the rocket. Each satellite has the shape of a partial cylinder segment of which an outer wall is a cylindrical segment shell. The satellites are bundled and secured together around the central structure by tension bands, whereby the cylindrical segment shells form a load-bearing complete outer cylindrical shell that surrounds the central tube. This structure provides sufficient stiffness and strength to withstand the loads that arise during launch, while having a reduced mass. The satellites themselves, rather than the central structure, bear the loads during launch. This allows the central structure to be of relatively lightweight construction.
摘要翻译：用于将多个卫星发射和分配到轨道的装置包括中央结构和可释放地捆绑在中心结构周围的多个卫星，以形成安装在发射器火箭的上级上的内聚单个有效载荷。中心结构包括中心管和适配器壳体，其适合于火箭的上部台阶。每个卫星具有部分气缸段的形状，其外壁是圆柱形段壳体。卫星通过张力带捆扎在一起并围绕中心结构固定在一起，由此圆柱形部分壳形成围绕中心管的承载完整的外圆柱形壳体。该结构提供足够的刚度和强度以承受发射期间产生的负载，同时具有减小的质量。卫星本身而不是中央结构在发射过程中承受负载。这使得中心结构的结构相对较轻。

2. 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。

3. 发明授权

US4690355A Solar energy collector 失效
标题翻译：太阳能收集器
公开(公告)号：US4690355A
公开(公告)日：1987-09-01
申请号：US918285
申请日：1986-10-10
申请人： Ernst Hornung , Dietrich Rex
发明人： Ernst Hornung , Dietrich Rex
IPC分类号： B64G1/22 , B64G1/44 , F24S23/70 , H01L31/054 , H02S20/32 , H02N6/00
CPC分类号： B64G1/443 , B64G1/222 , F24J2/10 , H01L31/0547 , H02S20/32 , F24J2002/1014 , F24J2002/108 , Y02E10/40 , Y02E10/52 , Y10S136/292
摘要： A solar energy collector arrangement is comprised of a plurality of parallely arranged strip-like mirrors, preferably made of aluminum with a silver layer on a concavely curved surface and solar cells being arranged on the rear convexly curved surface, upon which the mirror next to the first mentioned one concentrates solar radiation. These mirror strips are suspended by means of cable inbetween two bars so as to change the orientation of them vis-a-vis the sun; the bars, in turn, are preferably pivotably connected to a telescopic mast, there being additionally guide cable for gathering the individual mirrors. The entire arrangement can be pulled together by pulling all mirrors in juxtaposed position and pivoting the transverse bars against the telescopic mast.
摘要翻译：太阳能收集器装置由多个平行布置的带状反射镜构成，优选由铝制成，在凹曲面上具有银层，太阳能电池布置在后凸形曲面上，首先提到的一个是集中太阳辐射。这些镜带通过电缆悬挂在两个杆之间，以便改变它们相对于太阳的方向; 杠杆又优选地可枢转地连接到伸缩式桅杆，另外还有用于收集各个反射镜的引导电缆。通过将所有后视镜并列拉动并将横向杆枢转到可伸缩的桅杆上，整个布置可以被拉在一起。

4. 发明授权

US5520270A Tank structure for holding liquid especially in a spacecraft 失效
标题翻译：用于保持液体的坦克结构，特别是在航天器中
公开(公告)号：US5520270A
公开(公告)日：1996-05-28
申请号：US415422
申请日：1995-04-03
申请人： Ernst Hornung , Huba Oery , Herbert Wenz
发明人： Ernst Hornung , Huba Oery , Herbert Wenz
IPC分类号： B64D37/02 , B64G1/40 , F02K9/60 , F16F9/10
CPC分类号： B64D37/02 , B64G1/402 , B64G2001/228
摘要： Vibrations of pipes or other components installed in a container such as a tank intended for holding liquids, are damped by surface area damping bodies, e.g. plates with through-holes that are immersed in the liquid in the container. These plates are rigidly connected to the pipes or components to be damped. The vibration damping plates are constructed of metal, for example, and the through-holes reduce the mass and advantageously affect the damping effect. The materials for making the perforated damping plates are selected to be compatible with the content of the containers, such as a fuel in a tank in a spacecraft. The surface area ratio of all cross-sectional areas of the through-holes to the total plate surface area is optimized to achieve a maximum damping effect. These perforated plates are secured to pipes, braces, filters, ducts, or other internal components of fuel tanks of land vehicles, aircraft, and spacecraft.
摘要翻译：安装在诸如用于保持液体的罐的容器中的管道或其他部件的振动由表面积阻尼体阻尼，例如，具有浸没在容器中的液体中的通孔的板。这些板刚性连接到要阻尼的管道或部件上。振动阻尼板例如由金属构成，并且通孔减小质量并有利地影响阻尼效果。用于制造穿孔阻尼板的材料被选择为与容器的内容物（例如在航天器中的罐中的燃料）相容。通孔的所有横截面积与总板表面积的表面积比优化，以达到最大阻尼效果。这些多孔板被固定到陆地车辆，飞机和航天器的燃料箱的管道，支架，过滤器，管道或其他内部部件。

5. 发明授权

US5411349A Apparatus for coupling cylindrical structural components to each other 失效
标题翻译：用于将圆柱形结构部件彼此连接的装置
公开(公告)号：US5411349A
公开(公告)日：1995-05-02
申请号：US85756
申请日：1993-06-30
申请人： Ernst Hornung , Huba Oery , Stefan Hornung , Andreas Rittweger
发明人： Ernst Hornung , Huba Oery , Stefan Hornung , Andreas Rittweger
IPC分类号： B64G1/64 , F16B2/08 , F16L23/06 , F16L23/04
CPC分类号： B64G1/645 , B64G1/641 , F16B2/08 , F16L23/06 , Y10T292/212 , Y10T403/648
摘要： Cylindrical bodies of structural components, such as a spacecraft and a rocket section or two rocket sections, are coupled to each other by a releasable coupling device. The structural components have radially protruding flanges that face each other and are encircled by the coupling device. The coupling device includes a flexible tensioning element, such as a steel belt or link chain, the ends of which are interconnected by a clamping or locking device. The clamping or locking device is constructed as a two-armed lever, one end of which is connected to each of the ends of the tensioning element. The two-armed lever is rotatably supported and driven by an operating member such as a pipe section or rod. The two-armed lever is thus rotatable through an angle of about 180.degree. so that the ends of the tensioning element are brought into overlapping positions. When the ends are in such overlapping positions the device is locked. Rotation of the two-armed lever into the opposite direction unlocks the device.
摘要翻译：诸如航天器和火箭部分或两个火箭部分的结构部件的圆柱体通过可释放的联接装置彼此联接。结构部件具有径向突出的凸缘，其彼此面对并且被联接装置环绕。联接装置包括柔性张紧元件，例如钢带或连杆链，其端部通过夹紧或锁定装置相互连接。夹紧或锁定装置被构造为双臂，其一端连接到张紧元件的每个端部。双臂杠杆由诸如管段或杆的操作构件可旋转地支撑和驱动。双臂杠杆因此可旋转大约180度的角度，使得张紧元件的端部处于重叠位置。当端部处于这样的重叠位置时，装置被锁定。双臂杆向相反方向旋转可解锁设备。

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