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    • 2. 发明授权
    • Method and devices for propulsion
    • 推进方法和装置
    • US5965836A
    • 1999-10-12
    • US705160
    • 1996-08-29
    • Mikhail A. Rakov
    • Mikhail A. Rakov
    • F41A1/00F42B15/00F41A1/08F42B15/10
    • F42B15/00F41A1/00
    • A method provides for shooting a missile-rocket. The missile-rocket has two movable parts and a propellant. The propellant is disposed between the one movable part and the first end of the other movable part. The missile-rocket undergoes three phases of acceleration. During the first phase, the method includes the steps of activating the propellant, moving one of the movable parts in response to the activation of the propellant, and urging the one of the movable parts to engage the other one of the movable parts. During the second phase, the method includes the step of urging the other one of the movable parts in response to the engagement. During the third phase, the method includes the step of releasing gases formed by activating the propellant from the missile-rocket to further urge the missile-rocket. The movable parts are preferably a shell and a core. In one embodiment, the core is moved in response to the activation of the propellant and urged to engage the front end of the shell. The shell is urged in response to the core engaging the front end of the shell. Further urging of the core and the shell is by releasing gases formed by activating the propellant from a chamber formed by the core and the shell. In another embodiment, the shell is moved in response to the activation of the propellant and urged to engage the core. The core is urged in response to this engagement. Further urging of the core and the shell is again by releasing gases formed by activating the propellant from a chamber formed by the core and the shell.
    • 一种用于射击导弹火箭的方法。 导弹火箭有两个可动部分和推进剂。 推进剂设置在一个可移动部分和另一个可移动部分的第一端之间。 导弹火箭经历三个加速阶段。 在第一阶段期间,该方法包括以下步骤:启动推进剂,响应于推进剂的启动而移动可移动部件中的一个,并且推动可移动部件之一与另一个可移动部件接合。 在第二阶段期间,该方法包括响应于接合而推动另一个可移动部分的步骤。 在第三阶段,该方法包括释放通过从导弹火箭启动推进剂形成的气体以进一步推动导弹火箭的步骤。 可移动部件优选为壳体和芯部。 在一个实施例中,芯部响应于推进剂的激活而被移动并被推动以接合壳体的前端。 壳体响应于与壳体的前端接合的芯部被推动。 芯和壳的进一步推动是通过释放通过由由核和壳形成的室激活推进剂而形成的气体。 在另一个实施例中,壳体响应于推进剂的激活而被移动并被推动以接合核心。 为了回应这一参与,敦促核心。 核心和壳体的进一步推动是再次通过从由核心和壳体形成的腔室中激活推进剂而形成的气体。
    • 3. 发明授权
    • Release unit, and release system comprising at least one such release
unit
    • 释放单元和包括至少一个这样的释放单元的释放系统
    • US5381721A
    • 1995-01-17
    • US181960
    • 1994-01-18
    • Peter HolmstromSven Pettersson
    • Peter HolmstromSven Pettersson
    • B64D1/02F41F1/08F41H11/02F41A1/00F42B4/26
    • B64D1/02F41F1/08F41H11/02
    • A release unit for launching countermeasures from a vehicle. A first module in the form of a central body mounted on the vehicle. The first module includes at least three openings: a first opening facing the vehicle when the first module is mounted on the vehicle, and second and third openings directed obliquely with respect to the first opening in substantially opposite directions from each other. The directions the second and third openings face are separated by 60.degree.-120.degree.. A second module and a third module in the form of release cassettes are received respectively by the second and third openings and removably fixed by with a locking member. A plurality of countermeasures are launched from the release units. Each release cassette includes a plurality of countermeasure openings for receiving the countermeasures. The countermeasure openings in each cassette are aimed substantially in the same direction. A plurality of the countermeasures are launched to delimited spaces from each cassette, creating separate decoys without any movement of the release unit relative to the vehicle on which it is mounted. The countermeasures launched from the second module are launched away from the vehicle in substantially a first direction creating a first decoy and the countermeasures launched from the third module are launched away from the vehicle in substantially a second direction separated from said first direction by 60.degree.-120.degree. creating a second decoy. The first and second decoys are non-overlapping and separated from each other by a distance corresponding to the angle between the cassettes.
    • 用于从车辆发射对策的释放单元。 安装在车辆上的中心体形式的第一模块。 第一模块包括至少三个开口:当第一模块安装在车辆上时面向车辆的第一开口,以及相对于第一开口以基本上相反的方向倾斜地指向的第二和第三开口。 第二和第三开口面朝60°-120°分开。 剥离盒形式的第二模块和第三模块分别由第二和第三开口容纳并用锁定构件可拆卸地固定。 从释放单元启动多个对策。 每个释放盒包括用于接收对策的多个对策开口。 每个盒中的对策开口基本上瞄准相同的方向。 多个对策被发射到与每个盒子分隔开的空间,产生单独的诱饵,而没有释放单元相对于其上安装的车辆的任何移动。 从第二模块发射的对策在大致第一方向上从车辆开始,产生第一诱饵,并且从第三模块发射的对策从远离所述第一方向的第二方向远离车辆发射60度 - 120°造成第二个诱饵。 第一和第二诱饵不重叠并且彼此分开与盒之间的角度相对应的距离。
    • 9. 发明授权
    • Smart electronic muzzle reference light source
    • 智能电子枪口参考光源
    • US6072400A
    • 2000-06-06
    • US368466
    • 1999-07-15
    • Mark A. JohnsonPaul J. Cote
    • Mark A. JohnsonPaul J. Cote
    • F41A1/00G08B3/00
    • F41A1/00
    • An electronic light source which replaces the hazardous tritium light sou used in the existing Muzzle Reference System (MRS) found on the M1 Series of tanks. The MRS is mounted near the muzzle end of the gun (opposite the breech) and is used by tank gunness to measure gun deflection for calibration of the tank's fire control computer to optimize accuracy. The electronic light source is an LED which is activated by the pulses from a microcontroller based on the input received from a small, low power, omnidirectional motion sensor which detects the movement of the tank mounted on the tank. In the current implementation, the motion sensor comprises a conductive rolling sphere in a cylindrical chamber having a conductive wall with one electrical pole and end plates electrically insulated from the conductive wall and having the other electrical pole such that movement of the element caused by movement of the cylinder will generate intermittent electrical contact between one end plate and the cylinder wall. The signals produced are fed to the microcontroller which through the operation of its oscillator energizes the LED. The oscillator frequency is selected to eliminate EMI detection. The activation of the LED is prepared in such a manner to extend battery lite by minimizing power drain, a thermometer is employed for temperature control of the LED and other electronic circuit elements.
    • 一种电子光源,代替在M1系列坦克上发现的现有枪支参考系(MRS)中使用的危险氚光源。 MRS安装在枪口(枪口对面)的枪口附近,并通过坦克炮使用来测量枪偏转,以校准坦克的消防控制计算机以优化精度。 电子光源是由微控制器的脉冲基于从小的,低功率的全向运动传感器接收的输入激活的LED,其检测安装在罐上的罐的运动。 在当前的实现中,运动传感器包括在圆柱形腔室中的导电滚动球体,其具有导电壁,该导电壁具有一个电极和与导电壁电绝缘的端板,并且具有另一个电极,使得元件的移动 气缸将在一个端板和气缸壁之间产生间歇性电接触。 产生的信号馈送到微控制器,通过其振荡器的操作激励LED。 选择振荡器频率以消除EMI检测。 LED的激活以通过最小化功率消耗来延长电池容量的方式制备,温度计用于LED和其它电子电路元件的温度控制。