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71. 发明授权

US5904319A Guided missile with ram jet drive 失效
标题翻译：导弹与喷气式喷射机
公开(公告)号：US5904319A
公开(公告)日：1999-05-18
申请号：US919982
申请日：1997-08-28
申请人： Walter Hetzer
发明人： Walter Hetzer
IPC分类号： F42B10/64 , F02K7/10
CPC分类号： F42B10/64
摘要： A guided missile with ram jet drive, with an engine occupying the airframe cross section, with two outer air intakes in the lower area of the airframe, which lead to the tail with wake shafts, with a tail plane including four separately pivotable vanes in the form of a diagonal cross. A rigid wing arrangement is provided in or in front of the center of the missile. One drive unit with linear movement is provided for each vane. Two of the drive units are arranged longitudinally offset in the longitudinal and circumferential directions of the guided missile in each wake shaft. A kinematic connection from the drive unit to the lower vane is formed by a coupling rod each with joints at both ends. A kinematic connection from the drive unit to the upper vane is formed by a pivotable double lever each and a coupling rod with ball joints at both ends.
摘要翻译：具有喷射式喷射驱动的导弹，其中引擎占据机身横截面，机身下部区域具有两个外部进气口，其中尾部带有尾流轴，尾翼包括四个可分离的枢转叶片对角十字架的形式。导弹中心内或前面设有一个刚性翼结构。为每个叶片提供一个具有线性运动的驱动单元。两个驱动单元沿每个尾轴中的导弹的纵向和圆周方向纵向偏移地布置。从驱动单元到下叶片的运动学连接由两端具有接头的连接杆形成。从驱动单元到上叶片的运动学连接由可枢转的双杠杆和两端具有球接头的联接杆形成。

72. 发明授权

US5903192A Arrangement for controlling the output amplitude of a high frequency power amplifier 失效
标题翻译：用于控制高频功率放大器的输出幅度的装置
公开(公告)号：US5903192A
公开(公告)日：1999-05-11
申请号：US805242
申请日：1997-02-24
申请人： Michael Ludwig , Marcus Wahl
发明人： Michael Ludwig , Marcus Wahl
IPC分类号： H03G3/30
CPC分类号： H03G3/3052
摘要： A controlled, saturated high frequency power amplifier, which can be used especially as a transmitting amplifier in a T/R module for a phase-controlled (radar) antenna for the X-band (8 GHz to 12 GHz). In this case, a portion of the HF output signal is utilized to generate a control signal, with which the output power is controlled nearly without loss via at least one gate connection for the HF power amplifier components, preferably, field effect transistors, that are components of the power amplifier. The power amplifier thus has a high degree of transmitting effectiveness, even with a pulsed transmitting operation.
摘要翻译：一种受控的饱和高频功率放大器，可用于X波段（8 GHz至12 GHz）的相位控制（雷达）天线的T / R模块中的发射放大器。在这种情况下，HF输出信号的一部分被用于产生一个控制信号，通过至少一个用于HF功率放大器组件的栅极连接，输出功率几乎没有损耗被控制，优选地，场效应晶体管是功率放大器的组件。功率放大器因此具有高度的发射效率，即使采用脉冲发射操作。

73. 发明授权

US5899060A Wall structure for fuel-cooled rocket engine walls 失效
标题翻译：燃油冷却火箭发动机墙壁结构
公开(公告)号：US5899060A
公开(公告)日：1999-05-04
申请号：US787389
申请日：1997-01-22
申请人： Gunther Schmidt
发明人： Gunther Schmidt
IPC分类号： F02K9/64 , F02K9/97 , F02K99/00 , F02K11/00
CPC分类号： F02K9/64
摘要： A wall structure for fuel-cooled engine walls, with a cooling structure having an inner wall to which hot gas is admitted; an outer wall located at a spaced location therefrom; as well as a plurality of webs, which connect the two walls and divide the intermediate space between the walls into cooling channels (19), and with a support structure in the form of at least one stable outer jacket. The cooling structure is slotted from the outside in the area of each web, wherein the slots (22) pass through the outer walls and the centers of the webs into the area of the inner wall. The support structure is designed as an elastically nonrigid support structure at least in the area joining the cooling structure and/or is located at a spaced location from the cooling structure.
摘要翻译：用于燃料冷却的发动机壁的壁结构，具有冷却结构，其具有允许热气体的内壁; 位于其间隔开的位置的外壁; 以及连接两个壁并且将壁之间的中间空间分成冷却通道（19）并且具有至少一个稳定的外护套形式的支撑结构的多个腹板。冷却结构从每个腹板区域的外侧开槽，其中槽（22）穿过外壁和腹板的中心进入内壁的区域。支撑结构至少在连接冷却结构的区域和/或位于与冷却结构间隔开的位置处被设计为弹性非刚性支撑结构。

74. 发明授权

US5865207A Releasing means 失效
标题翻译：释放手段
公开(公告)号：US5865207A
公开(公告)日：1999-02-02
申请号：US734828
申请日：1996-10-22
申请人： Arno Voit , Gunter Langel
发明人： Arno Voit , Gunter Langel
IPC分类号： B64G1/40 , B64G1/64 , F02K9/58 , F16K17/16
CPC分类号： B64G1/402 , B64G1/645 , F02K9/58 , Y10S137/91 , Y10T137/1699 , Y10T137/1744 , Y10T137/1752
摘要： A releasing device for rocket fuel lines, arranged between a tank outlet and a shutoff valve, which releases the flow path at a defined, tank-side overpressure, with a piston-like bursting element. A disk is provided with a predetermined breaking point and with a clamping flange, as well as a guide rod that is rigidly attached to the disk, and a catching basket that is permeable to flow and fixes the disk in a positive-locking manner after rupture and axial movement. The bursting element is assembled by welding from two parts, namely, the disk with the clamping flange and the predetermined breaking point as one part, and the guide rod with the disk seat as the other part, the disk with the clamping flange is manufactured by machining from a cold-worked, weldable plate material with low breaking strength, the guide rod is manufactured by machining from the rod stock of which the disk was made or of a weldable material having a higher strength, and the predetermined breaking point is manufactured by machining as a one-sided notch on the side of the bursting element facing away from the tank.
摘要翻译：一种用于火箭燃料管线的释放装置，布置在罐出口和截止阀之间，其在限定的罐侧过压下释放流路，并具有活塞式爆破元件。盘具有预定的断裂点，并且具有夹紧凸缘，以及刚性地附接到盘的导向杆，以及在破裂之后可以以积极锁定方式流动和固定盘的捕获篮和轴向运动。爆破元件通过焊接从两部分组装，即具有夹紧法兰的盘和作为一部分的预定断裂点，并且具有作为另一部分的盘座的导杆，具有夹紧凸缘的盘由通过具有低断裂强度的冷加工可焊接板材进行加工，导杆通过从制造圆盘的棒料或具有较高强度的可焊接材料加工而制造，并且预定断裂点由在爆破元件的背离油箱的一侧作为单面槽口加工。

75. 发明授权

US5841071A Electrical conductor for a spacecraft solar generator 失效
标题翻译：航天器太阳能发电机用导体
公开(公告)号：US5841071A
公开(公告)日：1998-11-24
申请号：US567329
申请日：1995-12-05
申请人： Guenther La Roche , Christiane Oxynos-Lauschke
发明人： Guenther La Roche , Christiane Oxynos-Lauschke
IPC分类号： B23K11/20 , B64G1/44 , C22C5/02 , H01B1/02 , H01L31/02 , H01L31/05 , H01R4/00
CPC分类号： B64G1/443 , H01B1/02 , H01L31/02008 , H01L31/0512 , Y02E10/50
摘要： An electrical conductor for a spacecraft solar generator with at least one solar module, wherein the electrical conductor is made of an alloy containing gold and traces of at least one of silver, palladium or copper and which can be used as a solar cell connector. The electrical conductor advantageously cannot be oxidized by atomic oxygen, has a high hardness and elasticity and can thus withstand high thermal stresses. Furthermore, the electrical conductor can be processed by resistance welding without damaging the cell.
摘要翻译：一种用于具有至少一个太阳能模块的航天器太阳能发电机的电导体，其中所述电导体由含有金和痕量的银，钯或铜中的至少一种的合金制成，并且可用作太阳能电池连接器。电导体有利地不能被原子氧氧化，具有高的硬度和弹性，因此可以承受高的热应力。此外，电导体可以通过电阻焊接而不损坏电池。

76. 发明授权

US5787702A Propulsion plant operating on the basis of catalytic and/or chemical decomposition of a propellant 失效
标题翻译：在推进剂的催化和/或化学分解的基础上运行的推进装置
公开(公告)号：US5787702A
公开(公告)日：1998-08-04
申请号：US726083
申请日：1996-10-04
申请人： Peter Tiedtke , Josef Wiener
发明人： Peter Tiedtke , Josef Wiener
IPC分类号： B64G1/24 , F02K9/52 , F02K9/68 , F02K9/02
CPC分类号： F02K9/52
摘要： A propulsion plant operating on the basis of a catalytic and/or chemical decomposition of a liquid propellant, is equipped with a so-called aspirator ring (19) that covers the exit openings of the injection pipes (11), thereby screening these openings toward the decomposition chamber. The aspirator ring (19) is further enclosed by an aspirator screen (19A). The aspirator ring is constructed as a vaulted channel (20) in which the discharge bores (21) are arranged in a pattern that assures a uniform distribution of the propellant into the catalyst bed in the decomposition chamber. The aspirator screen (19A) is also formed with a channel and both the channel in the screen (19A) and the channel in the aspirator ring (19) preferably have a semicircular cross-section. The catalyst bed is divided into two separate beds so that the respective housing can also be divided so that subassemblies of the thruster may be built separately and then assembled. One subassembly includes the injection components and one catalyst bed in a first housing section (5) and the other subassembly includes a second catalyst bed in a respective housing section (6) and an expansion nozzle (13) connected to the second housing section (6).
摘要翻译：基于液体推进剂的催化和/或化学分解操作的推进装置配备有覆盖喷射管（11）的出口的所谓的吸气环（19），从而将这些开口朝向分解室。吸气器环（19）进一步被吸气器筛（19A）封闭。抽吸器环被构造为拱形通道（20），其中排放孔（21）以确保推进剂均匀分布到分解室中的催化剂床中的图案布置。抽吸器筛网（19A）还形成有通道，筛网（19A）中的通道和抽吸器环（19）中的通道两者优选具有半圆形横截面。催化剂床分成两个独立的床，使得相应的壳体也可以分开，使得推进器的子组件可以单独构建并且然后组装。一个子组件包括在第一壳体部分（5）中的注射部件和一个催化剂床，另一个子组件包括在相应的壳体部分（6）中的第二催化剂床和连接到第二壳体部分（6）的膨胀喷嘴（13））。

77. 发明授权

US5785275A Missile weapons system 失效
标题翻译：导弹武器系统
公开(公告)号：US5785275A
公开(公告)日：1998-07-28
申请号：US758144
申请日：1996-11-25
申请人： Manfred Hiebl
发明人： Manfred Hiebl
IPC分类号： F41G7/22 , F41G7/20
CPC分类号： F41G7/2293 , F41G7/2206 , F41G7/2213 , F41G7/2226 , F41G7/2253
摘要： A missile weapons system with a homing head optical system and an alignment processor, in which the visual field of the homing head is adjusted to the size of the target by handing over the target marking frame size to the homing head, which is equipped with a zoom lens, and the effect of parallax on the correlation is eliminated.
摘要翻译：具有归位头光学系统和对准处理器的导弹武器系统，其中通过将目标标记框架尺寸移交到配置有目标标记框架尺寸的归位头，将归位头的视野调整到目标的尺寸变焦镜头，消除视差对相关性的影响。

78. 发明授权

US5750917A Warhead 失效
标题翻译：弹头
公开(公告)号：US5750917A
公开(公告)日：1998-05-12
申请号：US489921
申请日：1990-02-26
申请人： Joachim Seckler , Klaus-Peter Geiss
发明人： Joachim Seckler , Klaus-Peter Geiss
IPC分类号： F42B12/18
CPC分类号： F42B12/18
摘要： In a tandem warhead, the preliminary shaped charge (5) is arranged at the front end of a spacer (9) which is displaceable toward the front in a guide (12) provided in the preliminary structure (13) of the warhead. Shearing pins (14) are provided for fixing the spacer (9) in the pushed in position. A pyrotechnical element (16) is fastened at the spacer (9). The spacer (9) is provided at its rear end with an annular element (28) which contacts the lining (3) of the main charge (1) in the pushed in position. A pressure space (32) is accordingly formed, so that a high pressure is achieved when the pyrotechnical element (16) is fired, whereupon a recoil occurs due to the propellant gases of the pyrotechnical element (14) flowing out through nozzles (25), which recoil ensures a gentle starting of the spacer (9) into the moved out position.
摘要翻译：在串联弹头中，预备成形装置（5）布置在间隔件（9）的前端，该间隔件可在设置在弹头的初步结构（13）中的引导件（12）中向前移动。提供剪切销（14）用于将间隔件（9）固定在被推入就位。烟火元件（16）紧固在间隔件（9）处。间隔件（9）在其后端处设置有环形元件（28），该环形元件（28）在被推入就位时接触主电荷（1）的衬里（3）。因此，形成压力空间（32），使得当烟火元件（16）被点燃时获得高压，于是由于烟火元件（14）的喷射气体通过喷嘴（25）流出而发生反冲，，这种反冲确保了将间隔件（9）轻轻地启动到移出位置。

79. 发明授权

US5710853A Coil form 失效
标题翻译：线圈形式
公开(公告)号：US5710853A
公开(公告)日：1998-01-20
申请号：US699727
申请日：1996-07-30
申请人： Wolfgang Von Hoessle , Kuno Roder , Elmar Albert
发明人： Wolfgang Von Hoessle , Kuno Roder , Elmar Albert
IPC分类号： B64C19/00 , B65H49/02 , B65H55/00 , B65H75/18 , F41G7/32 , F42B15/04 , G02B6/44 , G02B6/10
CPC分类号： B65H49/02 , B64C19/00 , B65H55/00 , B65H75/18 , F41G7/32 , F42B15/04 , G02B6/4457
摘要： A coil support and a winding arranged thereon, especially one including a fiber-optic waveguide, whose turns are mutually fixed by a binding agent. The binding agent drys while a volatile solvent diffuses off. The coil support is permeable to solvent and is designed such that it has essentially the same coefficient of thermal expansion as the winding. This achieves the uniform, thorough drying of the binding agent over the entire winding and reduces the risk of damage to the fiber-optic waveguide during the transportation and the unwinding of the winding in a coil form.
摘要翻译：线圈支撑件和布置在其上的线圈，特别是包括光纤波导的线圈，其匝由粘合剂相互固定。当挥发性溶剂扩散时，粘结剂干燥。线圈支撑件对溶剂是可渗透的，并且被设计成使得其具有与绕组基本上相同的热膨胀系数。这实现了整个绕组上的粘合剂的均匀，彻底的干燥，并降低了在卷绕体的输送和展开期间损坏光纤波导的风险。

80. 发明授权

US5684494A Reflector antenna, especially for a communications satellite 失效
标题翻译：反射天线，特别是通信卫星
公开(公告)号：US5684494A
公开(公告)日：1997-11-04
申请号：US574444
申请日：1995-12-15
申请人： Norbert Nathrath , Helmut Wolf , Ludwig Haas , Manfred Lieke , Detlev Blaschke
发明人： Norbert Nathrath , Helmut Wolf , Ludwig Haas , Manfred Lieke , Detlev Blaschke
IPC分类号： H01Q3/18 , H01Q3/20 , H01Q15/24 , H01Q13/00
CPC分类号： H01Q3/20 , H01Q15/24 , H01Q3/18
摘要： The invention provides a reflector antenna, especially for a communications satellite, having at least one fixed main reflector (102) with an essentially circular aperture. A fixed feed system (118) includes a horn radiator (108) with a rotationally symmetric radiation diagram and a fixed polarization direction. An auxiliary reflector may be arranged to be rotationally positionable around a main axis (E) and has a reflecting surface that is shaped as a partial surface of a nonrotationally symmetric ellipsoid with a low numerical eccentricity, which illuminates main reflector (102) elliptically with an ellipticity that is essentially constant regardless of the rotational position.
摘要翻译：本发明提供了一种特别用于通信卫星的反射器天线，其具有至少一个具有基本圆形孔径的固定主反射器（102）。固定进料系统（118）包括具有旋转对称辐射图和固定极化方向的喇叭辐射器（108）。辅助反射器可以布置成围绕主轴线（E）可旋转地定位，并且具有形状为具有低数值偏心的非对称对称椭圆体的局部表面的反射表面，该反射表面椭圆形地照射主反射器（102）无论旋转位置如何，椭圆度基本上是恒定的。

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