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    • 1. 发明授权
    • Apparatus for triggering a passive safety device for protecting
passengers in a vehicle
    • 用于触发用于保护车内乘客的被动安全装置的装置
    • US5157268A
    • 1992-10-20
    • US625741
    • 1990-12-11
    • Hans SpiesAlfons WoehrlPeter HoraGuenther Fendt
    • Hans SpiesAlfons WoehrlPeter HoraGuenther Fendt
    • B60R21/16B60R21/01H01H35/14
    • B60R21/0133B60R21/0132B60R2021/0011B60R2021/01322
    • A passive safety device (62) is triggered for protecting vehicle passengers in the event of a collision. The output signals of a signal acceleration sensor (1) are integrated to form a signal which triggers the deployment of the safety device when a threshold value for the integrated signal is exceeded and simultaneously additional criteria are met. These conditions are met in a simple circuit with a single acceleration sensor (1), so that the entire apparatus including the safety device (62) can be installed compactly in a steering wheel of a motor vehicle. In addition to a first signal evaluation channel in which the sensor signal is integrated once, there is at least one second signal evaluation channel including two integrators (20) and (23) in which the sensor signal is integrated twice to provide a distance signal that is evaluated by a further threshold value switch (24). The safety device (62) is only triggered if both the singly integrated signal and the doubly integrated signal exceed prescribed thresholds within a prescribed time period. Additionally, a rear collision impact recognition circuit and a hammer blow impact recognition circuit (31 to 36; 41, 28) is provided to block the triggering of the safety device. A rest circuit is also provided.
    • 被动安全装置(62)被触发以在碰撞的情况下保护车辆乘客。 信号加速度传感器(1)的输出信号被积分以形成当超过积分信号的阈值并且同时满足附加标准时触发安全装置展开的信号。 在具有单个加速度传感器(1)的简单电路中满足这些条件,使得包括安全装置(62)的整个设备可以紧凑地安装在机动车辆的方向盘中。 除了传感器信号被集成一次的第一信号评估通道之外,还存在至少一个第二信号评估通道,其包括两个积分器(20)和(23),其中传感器信号被集成两次以提供距离信号, 通过另外的阈值开关(24)来评估。 只有在单一积分信号和双重积分信号在规定时间内超过规定的阈值时,才触发安全装置(62)。 此外,提供后碰撞碰撞识别电路和锤击冲击识别电路(31〜36; 41,28)以阻止安全装置的触发。 还提供休息电路。
    • 4. 发明授权
    • Combination propulsion system for a flying craft
    • 飞行器组合推进系统
    • US5014508A
    • 1991-05-14
    • US494990
    • 1990-03-16
    • Hans Lifka
    • Hans Lifka
    • B64G1/00B64G1/40F02C3/073F02C3/13F02K3/072F02K7/16F02K7/18F02K9/48F02K9/74F02K9/78
    • B64G1/401F02C3/073F02C3/13F02K3/072F02K7/16F02K7/18F02K9/78B64G1/402
    • A combination engine for a flying craft capable of flying at speeds within a wide range from subsonic speeds to hypersonic speeds, is equipped with a rocket engine section that is independent of an atmospheric air supply, and a turbo air jet engine section having a compressor which is driven by a turbine that is also independent of an external air supply. The combination may further include extra fuel supply nozzles for operation as a ram jet which uses the same flow channel as the turbo air jet engine section. A gas generator equipped with two valving mechanisms is arranged coaxially with the rocket engine section. The valving mechanisms are controllable to open the gas generator chamber to the rocket combustion chamber while closing off gas flow to the turbo air jet section or vice versa. Either section can work alone or in parallel and simultaneously with the other section. Each turbine wheel forms with one compressor wheel a free wheeling rotor without any intermediate guide wheels, whereby the turbine blades extend either radially inwardly or radially outside of the compressor blades. A gas mixer or distributor is arranged downstream of the turbine and leads into the combustion chamber of the turbo or ram jet section to mix external air with the turbine propellant gases.
    • 用于能够以亚音速到超音速的广泛范围内飞行的飞行器的组合引擎配备有独立于大气供应的火箭发动机部分和具有压缩机的涡轮喷气发动机部分 由涡轮机驱动,涡轮机也独立于外部空气供应。 该组合可以进一步包括用作作为涡轮喷气发动机部分使用相同流动通道的冲压喷射器的额外的燃料供应喷嘴。 配备有两个阀机构的气体发生器与火箭发动机部分同轴布置。 阀门机构是可控制的,以将气体发生器室打开到火箭燃烧室,同时关闭到涡轮空气喷射部分的气流,反之亦然。 任何一个部分可以单独工作或与其他部分并行工作。 每个涡轮机叶轮与一个压缩机叶轮一起形成一个没有任何中间导向轮的空转轮,由此涡轮机叶片在压缩机叶片的径向向内或径向外延伸。 气体混合器或分配器布置在涡轮机的下游,并进入涡轮或冲压射流部分的燃烧室,以将外部空气与涡轮推进剂气体混合。
    • 5. 发明授权
    • Protection device for a fiber light conductor junction
    • 用于光纤导体结的保护装置
    • US5009474A
    • 1991-04-23
    • US434407
    • 1989-11-08
    • Ulrich WurmserJosef Meyer
    • Ulrich WurmserJosef Meyer
    • G02B6/38
    • G02B6/2558
    • The junction between two optical fiber light conductors is protected by a sleeve envelope which connects the protection coatings directly to each other. Tension resistent filler fibers are compressed by a shrink fit inside the sleeve envelope so that tension stress bypasses the light conductor fibers through the filler fibers. The sleeve envelope ends are shrink fitted to the protection coating. The highly tension resistant filler fibers, surrounding and bridging the junction, are tightly enclosed in the sleeve envelope by the shrink fit so that tension stress also passes through the filler fibers, thereby permitting the sleeve envelope to perform its protection function while the filler fibers provide the required strength.
    • 两个光纤光导体之间的连接处由套管外壳保护,套管外壳将保护涂层直接连接在一起。 拉伸阻力填料纤维通过收缩配合被压缩在套筒外壳内,使得拉伸应力通过填充纤维绕过光导体纤维。 套筒套管端部被收缩装配到保护涂层上。 围绕和桥接接头的高抗张力填料纤维通过收缩配合被紧密地封闭在套管外壳中,使得拉伸应力也通过填充纤维,从而允许套管外壳执行其保护功能,同时填充纤维提供 所需的力量。
    • 6. 发明授权
    • Process for data transmission by means of a geo-stationary satellite and
at least one sub-satellite
    • 通过地球静止卫星和至少一个子卫星进行数据传输的过程
    • US4985706A
    • 1991-01-15
    • US250622
    • 1988-10-17
    • Manfred Schukat
    • Manfred Schukat
    • H04B7/19H04B7/195H04L23/02
    • H04B7/195H04L23/02H04B7/19
    • A process for data transmission uses a geo-stationary satellite and at least one sub-satellite, the sub-satellites being placed on lower orbits. For the transmission of news, at least two data streams are transmitted with different powers. The first data stream, with a higher power is used for linking with the geo-stationary satellite (S.sub.1) and the other data streams are transmitted by means of PN (pseudo-noise) sequences for linking with the sub-satellites (S.sub.2). Two data transmissions thus take place in the same carrier frequency, but involving different satellites that are both within the visibility range of an earth station. This type of transmission using additional data streams of information is suitable for controlling and/or regulating the exchange of news between satellite-satellite and/or earth-satellite-earth or for controlling or regulating the orbit of the satellites.
    • PCT No.PCT / EP87 / 00804 Sec。 371日期:1988年10月17日 102(e)日期1988年10月17日PCT 1987年12月19日PCT公布。 出版物WO88 / 04866 日期:1988年6月30日。数据传输过程使用地球静止卫星和至少一个子卫星,子卫星被放置在下轨道上。 为了传送新闻,至少有两个数据流以不同的权力发送。 具有较高功率的第一数据流用于与地球静止卫星(S1)连接,并且其它数据流通过用于与子卫星连接的PN(伪噪声)序列发送(S2)。 因此,两个数据传输在相同的载波频率中发生,但涉及在地球站的可见范围内的不同的卫星。 使用附加信息数据流的这种类型的传输适用于控制和/或调节卫星 - 卫星和/或地球 - 地球之间的新闻的交换或用于控制或调节卫星的轨道。
    • 7. 发明授权
    • Electromagnetic beam switch especially for laser resonators
    • 电磁光束开关特别适用于激光谐振器
    • US4950051A
    • 1990-08-21
    • US399267
    • 1989-08-28
    • Udo BartonGerhard Ruf
    • Udo BartonGerhard Ruf
    • H01S3/10G21K1/04H01S3/106
    • H01S3/106
    • An electromagnetic beam switch for a laser resonator or generator, specifically for the guided or controlled transmission of light into a light conductor has two electrically controllable rotary magnets arranged in twin fashion for redundancy. Each rotary magnet operates a filter glass plate to tilt these plates into the beam path for interrupting the beam generation. The plates (13a, 13b) cooperate with respective switch contacts in corresponding switches (14, 15) arranged so that during activation, that is during switching-on, both rotary magnets (11, 12) are connected in parallel with each other. Upon completion of a "flight phase " or switch over phase the rotary magnets are automatically connected in series with each other to operate at half power as compared to the initial full power energizing phase. RC-components are arranged to prevent a constant activation of the magnets.
    • 用于激光谐振器或发生器的电磁束开关,专门用于将光引导或控制地传输到光导体中,具有两个以双重方式排列的电可控旋转磁体用于冗余。 每个旋转磁体操作一个过滤器玻璃板,以将这些板倾斜到光束路径中,以中断光束产生。 板(13a,13b)与相应的开关(14,15)中的相应开关触点配合,使得在启动期间,即在接通期间,两个旋转磁体(11,12)彼此并联连接。 在完成“飞行阶段”或切换相位时,旋转磁体彼此串联自动连接,以与初始全功率通电阶段相比工作在一半功率。 RC组件被布置成防止磁体的恒定的激活。
    • 9. 发明授权
    • Wall surface structure having an improved radiant heat discharge
capability
    • 壁面结构具有改善的辐射热放电能力
    • US4890454A
    • 1990-01-02
    • US331276
    • 1989-03-30
    • Guenther SchmidtPeter Schmid
    • Guenther SchmidtPeter Schmid
    • F02K9/64F28F9/20F28F13/18
    • F28F9/20F02K9/64F28F13/18F28F2245/06Y10S165/904
    • The wall of a structural component that is subject to high thermal and mechanical stress, such as a position control rocket drive, has a plurality of grooves in its surface for an improved heat discharge by radiation emission. The grooves are cut into the wall surface and have a substantially U-type cross-sectional shape with parallel sidewalls and a substantially rounded groove bottom. The heat emission efficiency is substantially improved by making the groove depth (t) to be about 100 .mu.m and the groove width (b) to be at least 20% of the groove depth, thus (t/b) is at least 5. Additionally, the maximally permissable groove shape tolerance over the entire groove length must be .+-.1 .mu.m and the smallest spacing between neighboring grooves is about 10 .mu.m.
    • 承受高热和机械应力的结构部件的壁,例如位置控制火箭驱动器,在其表面上具有多个凹槽,用于通过辐射发射改善热放电。 凹槽被切割成壁表面并且具有基本上U形的横截面形状,其具有平行的侧壁和基本上圆形的凹槽底部。 通过使槽深度(t)为约100μm,槽宽度(b)至少为槽深度的20%,从而(t / b)为5以上,可以显着提高发热效率。 另外,在整个槽长度上最大允许的槽形容差必须为+/-1μm,并且相邻槽之间的最小间隔为约10μm。