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1. 发明公开

CN107101541A 一种变质心球转子引信延期解除保险装置有权
公开(公告)号：CN107101541A
公开(公告)日：2017-08-29
申请号：CN201710380152.2
申请日：2017-05-25
申请人：南京理工大学
发明人：刘国旗 , 陆静 , 王炅
IPC分类号： F42C15/26 , F42C15/28
CPC分类号： F42C15/26 , F42C15/28
摘要：本发明公开了一种变质心球转子引信延期解除保险装置，包括引信体、球转子、变质心机构、开口环、后坐保险机构；所述引信体包括端盖和底座；所述球转子安装在端盖和底座之间的球形孔内；所述变质心机构包括永磁体、剪切销和球转子中的磁流变液；引信体内设有两个第三安装孔，两个第三安装孔位于球形孔的两侧，且两个第三安装孔的形心连线垂直于端盖的轴向；第三安装孔上下端分别位于端盖和底座中；两个永磁体分别设置在两个第三安装孔的上端；端盖下端径向上对称设有两个第四安装孔，第四安装孔轴线垂直于端盖轴线，第四安装孔与第三安装孔相通；剪切销位于第四安装孔内，剪切销与永磁体下端接触；磁流变液从储存室通过流道流向目标室；本发明装置是在变质心球转子延长了解除保险时间，增加了安全性。

2. 发明公开

EP1558892A4 AN ELECTRONIC DETONATING SYSTEM FOR A SUBMUNITION AND A METHOD FOR ARMING THE SYSTEM 审中-公开
标题翻译：电子点火系统，用于聚焦使系统子弹药和方法
公开(公告)号：EP1558892A4
公开(公告)日：2010-10-13
申请号：EP03759168
申请日：2003-11-04
申请人： ADVANCED MATERIAL ENGINEERING
发明人： WANG SHONG SHOU , PANG WENG SHIN
IPC分类号： F42C15/40 , F42C15/192 , F42C15/21 , F42C15/23 , F42C15/24 , F42C15/28
CPC分类号： F42C15/40 , F42C15/192 , F42C15/24 , F42C15/28

3. 发明公开

EP1558892A1 AN ELECTRONIC DETONATING SYSTEM FOR A SUBMUNITION AND A METHOD FOR ARMING THE SYSTEM 审中-公开
标题翻译：电子点火系统，用于聚焦使系统子弹药和方法
公开(公告)号：EP1558892A1
公开(公告)日：2005-08-03
申请号：EP03759168.2
申请日：2003-11-04
申请人： Advanced Material Engineering Pte Ltd
发明人： Wang, Shong Shou , Pang, Weng Shin
IPC分类号： F42C15/40 , F42C15/21
CPC分类号： F42C15/40 , F42C15/192 , F42C15/24 , F42C15/28
摘要： An electronic detonating system (10) for a submunition and a method for arming the system (10) are described. The system (10) has a system housing (12) and a rotor switch assembly (14) mounted to the system housing (12). The rotor switch assembly (14) has a rotor housing (16) with a spring mount (34), a rotor (18) mounted to the rotor housing (16), electronic switch circuitry (20) coupled to an electric detonator and mounted to the rotor (18), a rotor retaining pin (22) coupled to a catch (24) formed by the electronic switch circuitry (20) to thereby retain the rotor (18) in a safe mode prior to arming the system (10) after launching the submunition, and a torsion spring (26) mounted to the spring mount (34) to bias the rotor (18) towards an arming position of the system (10) upon disengagement of the rotor retaining pin (22) from the catch (22).

4. 发明公开

EP2914924A4 GAS CONTROLLED DELAY TIMING DEVICE 审中-公开
标题翻译： GASGESTEUERTEVERZÖGERUNGSZEITPLANUNGSVORRICHTUNG
公开(公告)号：EP2914924A4
公开(公告)日：2016-07-20
申请号：EP13872159
申请日：2013-11-01
申请人： BERGER RORY
发明人： BERGER RORY
IPC分类号： F42C9/06
CPC分类号： B65D83/207 , B65D83/26 , F42B12/50 , F42C9/06 , F42C15/28

5. 发明公开

EP2914924A2 GAS CONTROLLED DELAY TIMING DEVICE 审中-公开
标题翻译：气控延时定时装置
公开(公告)号：EP2914924A2
公开(公告)日：2015-09-09
申请号：EP13872159.2
申请日：2013-11-01
申请人： Berger, Rory
发明人： Berger, Rory
IPC分类号： F42C9/06
CPC分类号： B65D83/207 , B65D83/26 , F42B12/50 , F42C9/06 , F42C15/28
摘要： A delay release device that connects to an aerosol filled canister that releases the aerosol in a delayed manner. The device includes a main body with a first plunger assembly mounted on one end. Formed adjacent to the first plunger assembly is a first chamber filled with a compressed gas pressurized from 40 to 150 psi based on the time delay desired. In the main body adjacent to the first chamber is a second chamber and a third chamber. Located inside the third chamber is a second plunger with a hollow stem introduced into a top valve assembly on the canister. To activate, the first plunger assembly is pressed inward which activates a second valve disposed between the first and second chambers. The second valve allows compressed gas to flow slowly from the first chamber into the second chamber and into the third chamber. The increased air pressure in the upper portion of the third chamber exerts a downward force on the second plunger which forces the hollow stem into canister and causes the aerosol gas to be released into a lower discharge chamber and then through holes formed on the main body.

6. 发明授权

US12018913B2 Rocket armament launchable from a tubular launcher with an outside launcher non-ignition securing and motor separation during flight 有权
公开(公告)号：US12018913B2
公开(公告)日：2024-06-25
申请号：US17262607
申请日：2019-07-28
申请人： RAFAEL ADVANCED DEFENSE SYSTEMS LTD.
发明人： Nadav Tal , Yossi Teper , Evgeny Guller , Jakov Ziv
IPC分类号： F41F3/045 , F42B3/00 , F42B15/36 , F42B30/04 , F42B39/20 , F42C15/28 , F42C15/31
CPC分类号： F41F3/045 , F42B3/006 , F42B15/36 , F42B30/04 , F42B39/20 , F42C15/28 , F42C15/31
摘要： Rocket armament launchable from a tubular launcher with an outside launcher non-ignition securing and motor separation during flight and a method to prevent the ignition of the armaments rocket even in the event of actuation of the armaments pyrotechnic assembly, which normally serves to eject the armament from the launcher and to ignite its rocket motor, wherein the armament comprises a gas dispersion assembly, which when the armament is not encased in the tubular launcher, prevents the ignition of the rocket motor even if the armaments pyrotechnic assembly is actuated; and a cutting and separation assembly that is actuated by the pressure of the rocket motor gases for mechanically cutting a structural connection between the rocket motor and the armaments effective payload and separate them during their flight.

7. 发明授权

US3881419A Pyrotechnic initiator 失效
标题翻译：烟火引发剂
公开(公告)号：US3881419A
公开(公告)日：1975-05-06
申请号：US41250973
申请日：1973-11-02
申请人： US NAVY
发明人： BEA GAYLE A
IPC分类号： F42B3/10 , F42C15/28
CPC分类号： F42B3/10 , F42C15/28
摘要： A pyrotechnic initiator with an inherent out-of-line safe/arm feature. The initiator is comprised of a solenoid striker, a diaphragm located between a source of gas vapor and the striker, a secondary explosive, and an igniter. The solenoid punctures the diaphragm allowing the contents from the source of gas vapor to pass into an explosive chamber where a voltage from the igniter ignites the gas. The explosion caused thereby initiates the secondary explosive which produces the desired explosive output.
摘要翻译：具有固有外线安全/手臂功能的烟火启动器。起动器包括螺线管撞击器，位于气体源和撞击器之间的隔膜，次级炸药和点火器。螺线管对隔膜进行穿刺，使得来自气体蒸汽源的内容物进入爆炸室，在那里来自点火器的电压点燃气体。因此引起的爆炸发动产生所需爆炸输出的二次炸药。

8. 发明授权

US3631803A Ejector sensor fuze 失效
标题翻译：喷射传感器FUZE
公开(公告)号：US3631803A
公开(公告)日：1972-01-04
申请号：US3631803D
申请日：1968-04-24
申请人： US NAVY
发明人： DAVIS EDWARD J
IPC分类号： F42C5/02 , F42C15/184 , F42C15/28 , F42C15/29 , F42C5/00 , F42C15/00
CPC分类号： F42C15/28 , F42C5/02 , F42C15/184 , F42C15/29
摘要： A pneumatically operated fuze utilizing the force of the missile ejection position to break the hermetic seal and unlock the arming mechanism. The hermetic seal is a membrane covering the housing in which the fuze is mounted. The locking means are brackets which are straightened by the downward movement of the ejection piston. A bellows is then exposed to the dynamic pressure and expands causing the arming mechanism to arm.
摘要翻译：利用导弹喷射位置的力量的气动引信打破气密密封并解锁布防机构。气密密封是覆盖壳体的膜，其中安装引信。锁定装置是通过弹出活塞的向下运动而矫直的支架。然后将波纹管暴露于动态压力并膨胀，使得布防机构臂。

9. 发明授权

US3077160A G-actuated air controlled time delay 失效
标题翻译： G致动空气控制时间延迟
公开(公告)号：US3077160A
公开(公告)日：1963-02-12
申请号：US5510360
申请日：1960-09-09
申请人： WILLIAMS WILLIAM F
发明人： WILLIAMS WILLIAM F
IPC分类号： F42C9/06 , F42C15/24 , F42C15/28
CPC分类号： F42C9/06 , F42C15/24 , F42C15/28

10. 发明授权

US3073241A Safety device for the fuze of a gyrating missile during flight 失效
标题翻译：飞行期间旋转导弹引信的安全装置
公开(公告)号：US3073241A
公开(公告)日：1963-01-15
申请号：US84755859
申请日：1959-10-20
申请人： VALERCA ETS
发明人： JEAN ROSSELET
IPC分类号： F42C15/28
CPC分类号： F42C15/28

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