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1. 实用新型

JPS4834300U 失效
公开(公告)号：JPS4834300U
公开(公告)日：1973-04-24
申请号：JP7713971
申请日：1971-08-26
IPC分类号： F42B15/00 , B64G1/00 , F02K9/97 , B64G1/20 , F42B13/30

2. 实用新型

JPS5041300U 失效
公开(公告)号：JPS5041300U
公开(公告)日：1975-04-26
申请号：JP9474773
申请日：1973-08-10
IPC分类号： F42B15/00 , B64D7/08 , B64G99/00 , F42C15/40 , B64G9/00 , F42B13/30

3. 实用新型

JPS4943439Y1 失效
公开(公告)号：JPS4943439Y1
公开(公告)日：1974-11-28
申请号：JP5990970
申请日：1970-06-18
IPC分类号： F42B10/62 , F42B13/30

4. 发明授权

US4129268A Rockets including trajectory controls 失效
标题翻译：火箭包括轨迹控制
公开(公告)号：US4129268A
公开(公告)日：1978-12-12
申请号：US503838
申请日：1965-10-23
申请人： Willis F. Tibbetts
发明人： Willis F. Tibbetts
IPC分类号： F41G7/36 , F42B15/01 , G01C19/02 , F42B13/30
CPC分类号： G01C19/025 , F41G7/36 , F42B15/01
摘要： 1. A rocket comprising a rear section including a motor, a forward war head section, an intermediate trajectory control section, and a rotatable connection between said control and motor sections, a gyroscope and a gas generator mounted within said control section, the generator ahead of the gyroscope, said gas generator including ignition means, a first nozzle operable to deliver a wheel-driving gas stream to the wheel of said gyroscope, and a second nozzle operable to deliver an upward thrust in assistance of the flight of said rocket, the thrust being applied approximately in the zone of the center of gravity of said rocket, means operable in response to a predetermined set-back force exerted on said rocket during its launch to engage and support said wheel against said force only during the existence of said force, gyroscope caging means, and means to release said caging means in response to the operation of said generator.
摘要翻译： 1.一种火箭，包括后部，包括马达，前向战头部分，中间轨迹控制部分以及所述控制部分和马达部分之间的可旋转连接，安装在所述控制部分内的陀螺仪和气体发生器，所述气体发生器包括点火装置，可操作以将车轮驱动气流输送到所述陀螺仪的车轮的第一喷嘴;以及第二喷嘴，所述第二喷嘴可操作以在所述火箭的飞行协助下传递向上的推力，推力大致施加在所述火箭重心的区域中，该装置可在响应于在其发射期间施加在所述火箭上的预定的后退力而操作，仅在所述力的存在期间接合并支撑所述轮抵抗所述力，陀螺仪闭合装置，以及响应于所述发生器的操作释放所述笼式装置的装置。

5. 发明授权

US3721410A Rotating surveillance vehicle 失效
标题翻译：旋转监视车
公开(公告)号：US3721410A
公开(公告)日：1973-03-20
申请号：US3721410D
申请日：1962-08-29
申请人： US NAVY
发明人： ANSPACHER W
IPC分类号： F41G7/22 , G01C11/02 , F41G7/00 , F41G9/00 , F42B13/30
CPC分类号： G01C11/025 , F41G3/02 , F42B12/365 , F42B15/08
摘要： 1. A reconnaissance system capable of scanning an inaccessible target area and relaying the information to an observation point where it is displayed for visual observation comprising an infrared transducer means for converting detected infrared radiations into electrical signals proportional to the detected infrared radiations, transmitting means connected to said transducer means for transmitting electrical signals, rotating projectile means rotating at a predetermined rate enclosing said transmitting means and having said transducer means fixedly attached to the outer periphery of the projectile for scanning in a helical path the target area in a fixed rotating relationship with the projectile, at a rate equal to the rotating rate of said projectile receiving means for receiving and demodulating said electrical signals, and visual display means connected to said receiving means for converting electrical signals into a visual representation of the target area.

6. 发明授权

US4309003A Target seeking gyro 失效
标题翻译：目标追求陀螺仪
公开(公告)号：US4309003A
公开(公告)日：1982-01-05
申请号：US117699
申请日：1980-02-01
申请人： William B. McLean
发明人： William B. McLean
IPC分类号： F41G7/22 , F42B13/30
CPC分类号： F41G7/2293 , F41G7/2213 , F41G7/2253
摘要： A free spinning gyroscope is provided which has a spin axis, together with precession means for precessing the gyroscope. In addition, means are provided for detecting an electromagnetic field of energy and adapted to generate signals indicative of misalignment of the gyroscope spin axis with the energy field. Means are provided for utilizing the generated signals to directly control the precessing means to align the gyroscope spin axis with the electromagnetic field of energy.
摘要翻译：提供了具有旋转轴的自由旋转陀螺仪，以及进动陀螺仪的进动装置。另外，提供了用于检测能量的电磁场并适于产生指示陀螺仪旋转轴与能量场的未对准的信号的装置。提供了用于利用所产生的信号来直接控制进动装置以使陀螺仪旋转轴与能量的电磁场对准的装置。

7. 发明授权

US4262596A Overhead attack missile 失效
标题翻译：架空攻击导弹
公开(公告)号：US4262596A
公开(公告)日：1981-04-21
申请号：US952427
申请日：1978-10-18
申请人： Michel Allier , Didier Lursat
发明人： Michel Allier , Didier Lursat
IPC分类号： F42B12/10 , F42B12/12 , F42B12/14 , F42B13/30
CPC分类号： F42B12/14
摘要： A overhead attack missile for targets of little movement such as tanks or firing turrets is described. It comprises: at least one hollow charge, with a unidirectional radial action possessing a pyrotechnic dissymmetry means such as the off-centering of the detonator of the charge to preserve the straightness of the burst despite the movement of the missile and a guidance means to bring the missile, at the end its course, overhead of the target. The invention is applied to any stabilized or unmanned aerial weapons carrying war heads.
摘要翻译：描述了对于诸如坦克或发射炮塔之类的小动作目标的高空攻击导弹。它包括：至少有一个中空电荷，具有单向径向作用，具有烟火不对称的手段，例如导弹的雷管的偏心，以保持爆发的平直度，尽管导弹的移动和引导装置带来导弹，到最后的路线，目标的开销。本发明适用于携带战头的任何稳定的或无人驾驶的空中武器。

8. 发明授权

US4033525A Feedback PDM encoder and method for actuating a pneumatic actuator with a digital autopilot 失效
标题翻译：反馈PDM编码器和用于启动具有数字自动驾驶仪的气动执行器的方法
公开(公告)号：US4033525A
公开(公告)日：1977-07-05
申请号：US638476
申请日：1975-12-08
申请人： John P. Leonard , Robert E. Yates
发明人： John P. Leonard , Robert E. Yates
IPC分类号： F41G7/30 , G05D1/02 , G05D3/18 , F42B13/30
CPC分类号： F41G7/301 , G05D1/0202 , G05D3/18
摘要： A feedback PDM encoder and method is presented which permits utilization ofneumatic pulse duration modulation (PDM) actuators with potentiometer position pickoffs in a digital autopilot loop. The actuator is directly driven by a signal derived in the digital autopilot which is in the pulse duration modulation (PDM) format. This signal is derived within the autopilot digital computer using conventional digital techniques. Analog feedback from the potentiometer which indicates angular excursion of the actuator is formatted into a PDM format. This method yields all signals necessary to operate the actuator in a closed loop missile control system.
摘要翻译：提出了一种反馈PDM编码器和方法，其允许在数字自动驾驶仪环路中利用具有电位计位置传感器的气动脉冲持续时间调制（PDM）致动器。致动器由在数字自动驾驶仪中得到的信号直接驱动，该信号处于脉冲宽度调制（PDM）格式。该信号是使用传统的数字技术在自动驾驶仪数字计算机内导出的。来自电位计的模拟反馈表示执行器的角度偏移被格式化为PDM格式。该方法产生在闭环导弹控制系统中操作执行器所需的所有信号。

9. 发明授权

US3758052A System for accurately increasing the range of gun projectiles 失效
标题翻译：准确增加枪支范围的系统
公开(公告)号：US3758052A
公开(公告)日：1973-09-11
申请号：US3758052D
申请日：1969-07-09
申请人： US NAVY
发明人： MC ALEXANDER R , STOUT L
IPC分类号： F42B15/00 , F42C13/04 , F42B13/30
CPC分类号： F42B15/00 , F42C13/047
摘要： The present invention is a gun system which utilizes rocket assisted projectiles and accurately controls their placement. The projectile is fired by a gun and actual trajectory variables are compared in a computer with desired trajectory conditions. If there is a difference, the firing time of the rocket is altered to make the actual trajectory variable correspond to the desired condition. A radar system is utilized by the computer to obtain the trajectory information. A transmitter is connected to the computer to send the firing signal to a receiver mounted in the projectile.
摘要翻译：本发明是利用火箭辅助射弹并准确地控制其放置的枪系统。射弹由枪射击，实际轨迹变量在具有所需轨迹条件的计算机中进行比较。如果存在差异，则改变火箭的点火时间，使实际的轨迹变量对应于所需条件。计算机利用雷达系统获得轨迹信息。发射器连接到计算机以将发射信号发送到安装在射弹中的接收器。

10. 发明专利

DE3146645A1 未知
公开(公告)号：DE3146645A1
公开(公告)日：1983-06-01
申请号：DE3146645
申请日：1981-11-25
申请人： RHEINMETALL GMBH
发明人： BETHMANN KARL WILHELM DIPL ING , THEIS ULRICH DIPL PHYS DR ING
IPC分类号： F42B8/14 , F42B13/30 , F42B13/16
摘要： In ammunition, preferably for machine cannons, including a subcaliber stabilized projectile equipped with a body of tracer material and a stabilizing element, the heat released during combustion of the tracer material is utilized to drastically change the strength of the material of an element used to fasten the stabilizing element to the projectile. By being able to set the time of combustion and of the change in the material, the stabilizing element changes its position with respect to the projectile. The system or ammunition in question becomes unstable and drops to the ground.

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