公开(公告)号：US08602303B1

公开(公告)日：2013-12-10

申请号：US13851107

申请日：2013-03-27

Applicant: Beijing Mechanical Equipment Institute

Inventor： Xuchang Ding ,  Nuo Xu ,  Shengjie Wang ,  Yan Shen ,  Lianjun Wang ,  Xiaojun Wang ,  Jiahui Li ,  Hongliang Yan

IPC: G06G7/80

CPC classification number: G05D1/12 ,  F41G3/06 ,  F41G3/08 ,  F41G5/08 ,  F41H11/02

Abstract: Systems and methods based on firing table fitting allow interception of a small low-altitude low-velocity target. A system includes: a target detecting system, a directing control system, a launch control system, an interception execution system, a communication bus a, a communication bus b and a communication bus c. Firing table data under a standard working condition and fitting parameters under different working conditions are pre-stored in the system. Based on target flight data and environment condition parameters, a lead aiming point is predicted, a time sequence of each stage of a fight flow is controlled, and firing data are output to execute an interception by the launch control system. An interception operation is simplified, a ground control of a non-controlled bomb fight flow is realized, a single shot success probability of an interception system is increased, and an interception cost is reduced.

Abstract translation: 基于发射台配合的系统和方法允许拦截一个小的低空低速目标。 系统包括：目标检测系统，引导控制系统，发射控制系统，拦截执行系统，通信总线a，通信总线b和通信总线c。 在标准工作条件下对工作台数据进行烧结，并在不同工况下对配件参数进行预先存储。 根据目标飞行数据和环境条件参数，预测出目标点，控制战斗流程各阶段的时间序列，输出射击数据，执行发射控制系统的拦截。 截取操作简化，实现了非受控炸弹战斗流的地面控制，拦截系统的单次成功概率增加，拦截成本降低。

公开(公告)号：US08550346B2

公开(公告)日：2013-10-08

申请号：US13851101

申请日：2013-03-27

Applicant: Beijing Mechanical Equipment Institute

Inventor： Hao Liu ,  Shengjie Wang ,  Xuchang Ding ,  Xiaoming Wei ,  Shuyong Han ,  Xuyang Qiu ,  Kegang Chi ,  Yan Shen ,  Aifeng Chen ,  Yulong Tang

IPC: G06F19/00

CPC classification number: F41G3/06 ,  F41G3/14 ,  F41G5/08 ,  F41H11/02 ,  F41H13/0006

Abstract: Systems and methods allow for intercepting a small, low-altitude and low-velocity target. A system includes a detecting apparatus, a directing control apparatus, an aiming control apparatus, a launch control apparatus, a launching device, and an intercepting device. A method includes: searching and tracking a target by the detecting apparatus in a networking mode, or by the aiming control apparatus in a single-soldier mode; sending target information to the launch control apparatus; performing a trajectory calculation by the launch control apparatus; and launching the intercepting device by the launching device to intercept the target. A low-cost system with a short response time can thus be realized. The target falls with the net at a low velocity under a parachute, and this is desirable in a city environment.

Abstract translation: 系统和方法允许拦截小型，低空和低速目标。 系统包括检测装置，引导控制装置，瞄准控制装置，发射控制装置，发射装置和拦截装置。 一种方法包括：以组网方式由检测装置搜索和跟踪目标，或以单兵模式由目标控制装置进行跟踪; 向所述发射控制装置发送目标信息; 执行发射控制装置的轨迹计算; 并由发射装置发射拦截装置拦截目标。 因此可以实现具有短的响应时间的低成本系统。 目标在降落伞下以低速下降，这在城市环境中是可取的。

公开(公告)号：US08707847B2

公开(公告)日：2014-04-29

申请号：US14011729

申请日：2013-08-27

Applicant: Beijing Mechanical Equipment Institute

Inventor： Shengjie Wang ,  Yajun Chen ,  Xuyang Qiu ,  Aifeng Chen ,  Yulong Tang ,  Shuyong Han

IPC: F41A1/10

CPC classification number: F41A1/10

Abstract: A pollution-free liquid balancing device comprises a sealing bag (1), a front cover (2), a rear cover (3) and liquid balancing matter (4), wherein the sealing bag (1), the front cover (2) and the rear cover (3) are all plastic material. The sealing bag (1) is filled with the liquid balancing matter (4) inside, and plastically sealed under high temperature at both ends. The diameters of the front cover (2) and the rear cover (3) are matched with the inner diameter of a launch barrel (5), and the sealing bag (1) is provided between the front cover (2) and the rear cover (3). In an ordinary transportation state, the liquid balancing matter (4) is well sealed in the sealing bag (1), and a missile is launched forward by the propulsion of powder during launch, the sealing bag (1), the front cover (2) and the rear cover (3) crack instantaneously, and the liquid balancing matter (4) is ejected backward outside the barrel at high speed. The forward and backward impulses are similar or equal, thereby reducing or eliminating the impulse to the launch barrel (5) during launch. The device has a simple structure and uses the pollution-free liquid balancing matter (4), thus there is no pollution after launch.

Abstract translation: 一种无污染液体平衡装置，包括密封袋（1），前盖（2），后盖（3）和液体平衡物（4），其中密封袋（1），前盖（2） 后盖（3）均为塑胶材质。 密封袋（1）内部装有液体平衡物（4），两端在高温下进行塑性密封。 前盖（2）和后盖（3）的直径与发射筒（5）的内径相匹配，密封袋（1）设置在前盖（2）和后盖 （3）。 在普通运输状态下，液体平衡物（4）密封在密封袋（1）中，并且在发射期间通过粉末推进向前发射导弹，密封袋（1），前盖（2） ）和后盖（3）瞬间裂开，并且液体平衡物质（4）以高速向后喷射到筒体外部。 前进和后退冲程相似或相等，从而减少或消除在发射时对发射筒（5）的冲击。 该装置结构简单，使用无污染液体平衡物（4），发射后无污染。

公开(公告)号：US08720315B2

公开(公告)日：2014-05-13

申请号：US14010511

申请日：2013-08-26

Applicant: Beijing Mechanical Equipment Institute

Inventor： Hao Liu ,  Shuyong Han ,  Shengjie Wang ,  Xuyang Qiu ,  Aifeng Chen ,  Yulong Tang ,  Kegang Chi ,  Hejiu Wang ,  Chengshuai Su

IPC: F41H5/007

CPC classification number: F41H5/007 ,  F41H13/0006

Abstract: A combustion gas piston type movable guiding tube netting device includes a capture net (8), a traction head (6), a guiding tube (7), an igniter (3), a main gunpowder (5), a combustion gas generator (1) and a piston (2). The piston and the main gunpowder are placed in the combustion gas generator. The top of the piston contacts a triangular lug on the base of the guiding tube. The traction head is placed in the guiding tube, and another end of the traction head is tied on one corner of the capture net. When operating, the main gunpowder is ignited by the igniter, the resulting combustion gas pushes the piston to move, the piston pushes the guiding tube to move, and the combustion gas comes into the guiding tube and pushes the traction head to burst out the guiding tube, and the traction head drives the capture net to open. The combustion gas piston type movable guiding tube netting device has a quick expansion speed, and the area of the expansive capture net is big.

Abstract translation: 燃烧气体活塞式可动引导管网装置包括捕集网（8），牵引头（6），引导管（7），点火器（3），主火药（5），燃烧气体发生器 1）和活塞（2）。 活塞和主火药放置在燃烧气体发生器中。 活塞的顶部与导管底部的三角形凸耳接触。 牵引头被放置在引导管中，牵引头的另一端被绑在捕获网的一个角上。 当操作时，主火药被点火器点燃，所产生的燃烧气体推动活塞移动，活塞推动导管移动，燃烧气体进入引导管并推动牵引头，使引导器 管，牵引头驱动捕获网打开。 燃气式活塞式可动引导管网装置具有快速的膨胀速度，膨胀捕获网面积大。