| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 一种电磁惯性复合转子式隔离机构 | CN201710498552.3 | 2017-06-27 | CN107121033A | 2017-09-01 | 李响; 倪竞华; 刘育 |
| 本发明公开了一种电磁惯性复合转子式隔离机构，属于引信保险机构技术领域。该隔离机构包括开设转子孔的本体，以及套嵌入转子孔中的转子，转子和本体上开设有容置电磁推销器、惯性保险部件、锁销、转换开关、传火部件、传爆部件等部件的孔洞，通过优选结构部件和优化孔洞位置，既使隔离机构具有较大的解除隔离转角，又能精确识别并反馈隔离机构所处的状态，且保证隔离机构在各状态下均能锁定在该状态。本发明通过上述设置，一方面确保了安全状态下的机构安全性，保证了待发状态下引爆序列的对正，大大提升了引爆效率；另一方面，转换开关等部件的应用能有效识别隔离机构所处的状态并反馈给控制系统，能进一步提升隔离机构的安全性和引爆效率。 | ||||||
| 2 | 一种热熔合金惯性复合转子式隔离机构 | CN201710498556.1 | 2017-06-27 | CN107121034A | 2017-09-01 | 李响; 陈亮; 雷林 |
| 本发明公开了一种热熔合金惯性复合转子式隔离机构，属于引信保险机构技术领域。该隔离机构包括开设转子孔的本体，以及套嵌入转子孔中的转子，转子和本体上开设有容置热熔合金推销器、惯性保险部件、锁销、转换开关、传火部件、传爆部件等部件的孔洞，通过优选结构部件和优化孔洞位置，既使隔离机构具有较大的解除隔离转角，又能精确识别并反馈隔离机构所处的状态，且保证隔离机构在各状态下均能锁定在该状态。本发明通过上述设置，一方面确保了安全状态下的机构安全性，保证了待发状态下引爆序列的对正，大大提升了引爆效率；另一方面，转换开关等部件能有效识别隔离机构所处的状态并反馈给控制系统，能进一步提升隔离机构的安全性和引爆效率。 | ||||||
| 3 | 高炮防雹增雨弹时间起爆引信 | CN201610952063.6 | 2016-10-27 | CN106338224A | 2017-01-18 | 王雨时; 闻泉 |
| 本发明公开一种高炮防雹增雨弹时间起爆引信，包括引信体(1)、覆盖于引信体(1)前端的风帽(2)及置于引信体(1)腔体内的发火机构机构(5)和传爆管(6)，所述发火机构(3)位于引信体(1)前部，所述实现延时功能的药盘延时机构(4)位于发火机构(3)与球转子保险和解除保险机构(5)之间，所述传爆管(6)前端与球转子保险和解除保险机构(5)相连，后端作为引信输出端，用于起爆含碘化银药柱的弹丸装药。本发明的高炮防雹增雨弹时间起爆引信，可靠性高、安全性好。(3)、药盘延时机构(4)、球转子保险和解除保险 | ||||||
| 4 | 一种引信解保试验装置 | CN201610665115.1 | 2016-08-12 | CN106123711A | 2016-11-16 | 赵颖涛 |
| 本发明公开了一种引信解保试验装置，包括机体和离心主轴，离心主轴转动安装在机体上，离心主轴下部设有传动轮，传动轮上连接有传动带，离心主轴上部固定有夹具，夹具内固定有引信，离心主轴为空心结构，拔销轴沿轴向穿过离心主轴，离心主轴上沿轴向设有长条孔，拔销轴和离心主轴经穿过长条孔的连接件相连接，拔销轴的上端设有挡销，挡销与引信底部设置的销孔配合，拔销轴下端设置有轴承座，拔销轴与轴承座转动连接，机体的底部安装有电磁铁，电磁铁的电磁铁芯与轴承座相连接。本发明通过电磁铁拖动轴承座实现垂直位移，完成了在高速环境下的引线的机械拔销，配合离心机的高速旋转，实现了引线在两种环境作用下的解保测试。 | ||||||
| 5 | 一种具有两级形状记忆合金保险的引信安保机构及引信 | CN201610120822.2 | 2016-03-03 | CN105783615A | 2016-07-20 | 李响; 姚宝珍; 贺政军 |
| 本发明公开了一种引信安保机构，包括质量杆、第一圆环、导爆药、管壳、保险销、弹簧、第一压螺、第二圆环、第二压螺；质量杆的中部套有材料为TiNi形状记忆合金的第一圆环；质量杆的下端连接导爆药，导爆药的外部装有管壳；质量杆的上方安装有第一压螺；质量杆的上部侧面开孔用于横向插入保险销，保险销的杆部套有弹簧，与保险销相邻且同轴地设有材料为TiNi形状记忆合金的第二圆环，第二圆环远离保险销的端部设有第二压螺。本发明还提供了包括上述引信安保机构的引信。本发明将驱动与执行一体化，大大减小整体结构尺寸，结构紧凑，工作可靠性高，解决了现有引信安保机构径向尺寸大、不适应于径向尺寸要求小场合。 | ||||||
| 6 | 一种具有自锁功能的引信安保机构及引信 | CN201610120668.9 | 2016-03-03 | CN105758268A | 2016-07-13 | 李响; 邬学聪; 魏梦颖 |
| 本发明提供一种具有自锁功能的引信安保机构，包括套筒、瓦片、质量杆、导爆药、管壳和保险机构；质量杆中部具有台阶，质量杆的台阶以上部分装有套筒，套筒内部周向均匀分布有多块瓦片，质量杆的上端安装保险机构，质量杆的下端连接导爆药，导爆药的外部装有管壳；工作时，解除保险机构的保险，当质量杆感受到过载，质量杆及与之连接的导爆药和管壳一起向下运动到限定位置，同时瓦片失去支撑向下滑落直至重新获得质量杆的中部台阶支撑，从而将质量杆锁定在限定位置。本发明还提供基于上述机构的引信。本发明利用飞行过载驱动安保机构，无需利用引信或弹上电源驱动；具有自锁功能，可靠性高；结构紧凑，适用于径向尺寸要求小的引信使用场合。 | ||||||
| 7 | JPS4943440B1 - | JP5767070 | 1970-07-01 | JPS4943440B1 | 1974-11-21 | |
| 8 | PROJECTILE STABILISE MIS EN OEUVRE SUR TRAJECTOIRE, NOTAMMENT LEURRE | EP07820558.0 | 2007-09-25 | EP2082183A1 | 2009-07-29 | PIGNOL, Marc; ESTIBALS, Olivier; MONTACQ, Cyril |
| The present invention relates to a device comprising at least one stabilized projectile (200, 300) housing an active element (210, 310) designed to generate a controlled technical effect over a trajectory, aerodynamic means (230, 330) that can be deployed between a rest retracted position in storage and deployed operational position over the trajectory, and safety means (224, 234) inserted between an initiation means (228, 280) and the active element (210, 310) to prevent the latter from being initiated until after the aerodynamic means (230, 330) have been deployed. | ||||||
| 9 | Dispositif de sécurité et d'armement pour engin explosif | EP94401182.4 | 1994-05-30 | EP0633449B1 | 1998-07-29 | Lemonnier, Georges; Duparc, Jean-Paul; Dussol, Jean-Pierre; Rebeyrol, Gilles |
| 10 | Projectile for smooth bore weapon | EP89309902.8 | 1989-09-28 | EP0363079B1 | 1994-07-13 | Shaphyr, Shalom |
| 11 | Projectile for smooth bore weapon | EP89309902.8 | 1989-09-28 | EP0363079A2 | 1990-04-11 | Shaphyr, Shalom |
The invention provides a projectile (1) adapted to be fired from a weapon, preferably from a cartridge with a propellant charge therein, wherein the projectile (1) comprises a generally cylindrical casing (3) and a warhead assembly (2), said warhead being hollow to accommodate an explosive charge (15) and an initiator (14), the casing being formed with a firing pin (4) spring biased (5) to a safety position and locked in safety position by a spring biased safety pin (6), wherein the spring biased safety pin is adapted to release on exit from the weapon, and wherein said casing includes a plurality of fins (8) foldable within the cartridge, but which deploy radially on leaving the weapon. The invention allows the projectile to be fired from a smooth bore weapon, such as a shotgun. The invention also provides an arming time delay mechanism to ensure that the projectile is only armed when at a safe distance from the operator. |
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| 12 | ROCKER ARM DETONATOR | US15185563 | 2016-06-17 | US20170363400A1 | 2017-12-21 | Helge GRAF |
| A rocker arm detonator is provided that includes a detonator head, which includes a pivotably arranged firing pin which is acted upon by a firing pin spring, and has a safety clip, which is pivotably disposed in the same direction of rotation as the firing pin from a starting position, in which it is pressed in the direction of the detonator head to a firing pin release position. To reliably avoid an unintentional detonation of the rocker arm detonator prior to its proper use, when the rocker arm detonator is not in use, the firing pin spring is in its untensioned state and may be tensioned by a separate tensioning lever as soon as the rocker arm detonator is to be properly deployed. | ||||||
| 13 | Rocker arm detonator | US15185563 | 2016-06-17 | US09846019B1 | 2017-12-19 | Helge Graf |
| A rocker arm detonator is provided that includes a detonator head, which includes a pivotably arranged firing pin which is acted upon by a firing pin spring, and has a safety clip, which is pivotably disposed in the same direction of rotation as the firing pin from a starting position, in which it is pressed in the direction of the detonator head to a firing pin release position. To reliably avoid an unintentional detonation of the rocker arm detonator prior to its proper use, when the rocker arm detonator is not in use, the firing pin spring is in its untensioned state and may be tensioned by a separate tensioning lever as soon as the rocker arm detonator is to be properly deployed. | ||||||
| 14 | Dual safety fuze for grenade | US14462702 | 2014-08-19 | US09638503B1 | 2017-05-02 | William J. Andrews; Carl J. Campagnuolo |
| A hand grenade fuze includes a secondary safety feature in the form of a trigger pin inserted through the striker lever. One end of the trigger pin has an undercut portion. A slide bar is disposed in the fuze body and has a keyhole opening at one end for selectively engaging the undercut portion of the trigger pin. A trigger has one end connected to the slide bar and another end rotatably fixed to the fuze body. A spring biases the trigger away from the fuze body. When the trigger is depressed, the slide bar translates and releases the trigger pin, which releases the restraint on the striker lever. | ||||||
| 15 | System for self destruction of a carrier shell submunition by chemical attack | US070220 | 1993-06-02 | US5373790A | 1994-12-20 | Patrice H. Chemiere; Jean-Paul A. Dupuy; Bernard F. Bayard; Jean-Pierre Ruet |
| A mechanical system for self-destruction of a munition, in particular a carrier shell submunition, is provided in a munition having a warhead initiated by a pyrotechnic sequence, a main striker and a priming device composed of a slide movable between a safety position and an armed position and which has a device for priming the charge. The self destruction system includes a secondary striker mounted inside a receptacle of a slide and a control device to release the secondary striker after a preset delay. Secondary striker is integral with a holding element and held abutting a seat by the urging of an arming spring. The control device of the secondary striker has a corrosive agent designed to chemically attack the holding element to release it from its seat. When the holding element is released, secondary striker is translationally moved to contact the detonator to destroy the munition. | ||||||
| 16 | Safe/arm explosive transfer mechanism | US833640 | 1986-02-25 | US4667600A | 1987-05-26 | Norman E. Jensen; Bennett W. Kelley |
| A safe/arm mechanism for an air-delivered explosive device uses a slider containing explosive leads as the means of interrupting the explosive train. The slider is locked in the safe position such that the explosive leads are out-of-line with respect to the detonator. The slider is attached directly to the main parachute such that when two locks are removed the parachute deployment forces can overcome a shear pin lock and move the slider to an in-line or armed position where it is positively retained. In this position, initiation of the detonator will allow the explosive output of the detonator to be transferred to its associated explosive device and provide a dual point radial initiation of its booster charge. | ||||||
| 17 | Method of payload delivery at low altitude | US444579 | 1974-02-21 | US3951069A | 1976-04-20 | Aaron S. Berlin; Vincent C. Little |
| A method of assembling munitions and delivering a payload within a munitiono a target area at low altitude wherein the energy source for arming the fuze is self contained within the mechanism and utilized subsequent to release of the munition from the delivery means. | ||||||
| 18 | Automatic porting mechanism | US45093974 | 1974-03-13 | US3894491A | 1975-07-15 | TIEMANN RALPH A |
| An automatic porting mechanism on a launchable device for latching a bore rider when said device is moved in one direction and for unlatching a bore rider when said device is moved in an opposite direction. The bore rider is pivotally attached to a slidable plug which closes an orifice in the launchable device. A lip on the bore rider is engageable with a shoulder adjacent the orifice to prevent ejection of the bore rider until forward movement of the device relative to a launcher unlatches the bore rider.
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| 19 | Safety wire interrupter assembly | US32225973 | 1973-01-09 | US3828645A | 1974-08-13 | TESTERMAN J; ROBERTSON L |
| An improved safety wire interrupter and method of arming munitions wherein a plastic member, such as high or low density polyethylene, is fused onto the safety wire to prevent withdrawal of the safety wire from a safety pin until tension is applied to a lanyard means fixedly connected to the safety wire.
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| 20 | Electrical delay arming always impact fuze | US3618524D | 1968-09-04 | US3618524A | 1971-11-09 | BERLIN AARON S; LITTLE VINCENT C |
| A fuze, method, and system for arming munitions for low altitude delivery wherein the energy source for arming the fuze is selfcontained within the mechanism and utilized subsequent to release of the munition from the delivery means.
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