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1. 发明公开

EP2697811A4 CHANGING THE STATE OF A SWITCH THROUGH THE APPLICATION OF POWER 审中-公开
标题翻译：通过使用性能改变开关状态
公开(公告)号：EP2697811A4
公开(公告)日：2014-11-26
申请号：EP11866905
申请日：2011-10-11
申请人： HALLIBURTON ENERGY SERV INC
发明人： BONAVIDES CLOVIS S
IPC分类号： H01H61/02 , F42C15/36 , F42C15/40 , F42C19/00 , H01H37/76 , H01H61/04
CPC分类号： H01H5/04 , F42C15/36 , F42C15/40 , F42C19/00 , H01H3/30 , H01H37/76 , H01H37/761 , H01H37/767 , H01H61/02 , H01H61/04 , H01H85/36 , H01H85/46 , H01H2037/762 , H01H2037/763

2. 发明公开

EP2153162A2 CHAINE PYROTECHNIQUE D'ALLUMAGE D'UNE CHARGE PRINCIPALE DE PROPULSION D'UN MISSILE 有权转让
标题翻译：烟火链主传动装药火箭点火
公开(公告)号：EP2153162A2
公开(公告)日：2010-02-17
申请号：EP08805914.2
申请日：2008-06-03
申请人： Snecma Propulsion Solide
发明人： BIZ, Philippe
IPC分类号： F42C15/184 , F42C15/24 , F42C15/34 , F42C15/36
CPC分类号： F42C15/184 , F42C15/24 , F42C15/34 , F42C15/36
摘要： The firing chain of the invention includes an arming device (40) mobile between a rest and an active position., two locking members (14, 16) for locking the arming device in a rest position and an active position, an arming pyrotechnical retarder (22), a squib (26) ignited at the ejection of the missile and igniting the arming retarder and releasing the first locking member (14) in order to allow the arming device to be switched into an active position, and a trajectory pyrotechnical retarder (32). A first relay charge (29) is adapted to be ignited at the end of the combustion of the arming retarder and to trigger the ignition of the trajectory retarder and the actuation of the second locking member (16) for locking the arming device in an active position and a second relay charge (34) is adapted to be ignited at the end of the combustion of the trajectory retarder and to trigger the ignition of the main charge.

3. 发明公开

EP3918270A1 SHOCK TUBE EVENT VALIDATION 有权
公开(公告)号：EP3918270A1
公开(公告)日：2021-12-08
申请号：EP20709114.1
申请日：2020-01-24
申请人： Detnet South Africa (Pty) Ltd
发明人： KRUGER, Michiel Jacobus , MAURISSENS, Daniel Auguste , KOEKEMOER, Andre Louis , LABUSCHAGNE, Albertus Abraham
IPC分类号： F42D1/04 , F42C15/36 , F42C15/40 , F42D1/045

4. 发明公开

EP2335012A1 EXPLOSIVE PART WITH SELECTABLE INITIATION 审中-公开
标题翻译：具有可选择射击炸药PART
公开(公告)号：EP2335012A1
公开(公告)日：2011-06-22
申请号：EP09813300.2
申请日：2009-08-18
申请人： BAE Systems Bofors AB
发明人： THUMAN, Christer
IPC分类号： F42C15/36 , F42B12/56 , F42B3/22 , F42C15/42 , F42C15/44
CPC分类号： F42B3/22 , F42B12/56 , F42C15/36 , F42C15/44
摘要： The invention is characterized in that the a explosive part (1) comprises two initiation devices (7) arranged on each end face (5) with connections to an inner explosive charge (2), the two initiation devices (7) being arranged for optional initiation of the inner explosive charge (2), with or without an ignition delay. At, and in that the diameter di of the inner explosive charge (2), the thicknesses ti, ty of the two insulating layers (8, 9) and thickness ts of air gap (10) are chosen such that energy from two colliding detonation fronts along the common centre axis A-A is required in order for the initiation to lead to detonation of the outer explosive charge (3). The invention also relates to a method for the above.

5. 发明授权

EP0381753B1 A THERMALLY INITIATED MECHANICALLY FIRED DEVICE FOR PROVIDING PROTECTION AGAINST SLOW COOK-OFF 失效
标题翻译：一种用于提供防止慢速烹饪的保护装置的热启动式机械装置
公开(公告)号：EP0381753B1
公开(公告)日：1993-06-16
申请号：EP89910773.4
申请日：1989-06-19
申请人： Hughes Aircraft Company
发明人： DOLAN, Cyril, F.
IPC分类号： F02K9/38 , F42C15/36 , F42B39/20
CPC分类号： F42C15/36 , F02K9/38 , F42B39/20
摘要： Slow cook-off protection for rocket motors is achieved through the use of a slow cook-off trigger mechanism (10) in which a mechanical response is thermally initiated. A metallic housing (12) contains and is thermally coupled to a bimetallic snap action disc spring (14). A firing pin (24) is connected to the disc spring and telescopically guided by the housing toward an explosive booster charge (40). The booster charge is coupled in a conventional manner to a linear shaped charge (52). The linear shaped charge is disposed adjacent to the rocket motor case in order to cut a stress riser in the casing when activated. The circular bimetallic spring is designed to snap between a first and second configuration to thereby drive the firing pin into the explosive booster charge at a predetermined temperature below the expected ignition temperature of the rocket propellant.

6. 发明公开

EP0456484A1 Temperature sensitive device 失效
标题翻译：温度变化Einrichtung。
公开(公告)号：EP0456484A1
公开(公告)日：1991-11-13
申请号：EP91304158.8
申请日：1991-05-09
申请人： GEC-MARCONI LIMITED
发明人： Lewis, John Dudley
IPC分类号： F42C15/36
CPC分类号： F42C15/36
摘要： A temperature sensitive firing device comprising a cylinder 12 having a frangible container 18 of a volatile liquid such as ethyl chloride therein; a piston 14 mounted in the cylinder 12 having a firing pin 20 mounted thereon and being held in place by releasable securing means 16 such as a shear pin; and detonator 22 spaced from the firing pin 20 by a fusible member 24 such as a collar made of a eutectic alloy.
摘要翻译：一种温度敏感的点火装置，包括：气缸12，其中具有诸如乙基氯的挥发性液体的易碎容器18; 安装在气缸12中的活塞14具有安装在其上的击发销20并且通过诸如剪切销的可释放的固定装置16保持就位; 并且由诸如由共晶合金制成的套环的可熔部件24与击发销20间隔开的雷管22。

7. 发明公开

EP3129743A4 ARRANGEMENT FOR LOCKING ARMING CONDITIONS 有权
公开(公告)号：EP3129743A4
公开(公告)日：2017-11-15
申请号：EP14888956
申请日：2014-04-11
申请人： SAAB AB
发明人： ANDERSSON BENGT , KARLSSON PER , STRAND FILIP
IPC分类号： F42C15/24 , F42C15/18 , F42C15/32 , F42C15/36
CPC分类号： F42C15/24 , F42C15/32 , F42C15/36
摘要： An arrangement for locking arming conditions to prevent unintentional arming of SAI-units of ammunition units when the ammunition unit is subjected to external threats. A ring shaped shape memory alloy is provided in cooperation with a recess in a plunger arranged in connection to the SAI-unit and a fixed recess to prevent the plunger from axial movement when subjected to heating by changing the shape of the essentially ring shaped shape memory alloy to lock the plunger relative to the fixed recess.

8. 发明公开

EP2219741A1 THERMISCHER AUSLÖSEMECHANISMUS MIT EINER GLASAMPULLE FÜR AEROSOL-FEUERLÖSCHGENERATOREN 有权
标题翻译：与玻璃安瓿气溶胶火灾发电机热脱扣机构
公开(公告)号：EP2219741A1
公开(公告)日：2010-08-25
申请号：EP08857565.9
申请日：2008-12-04
申请人： Dynamit Nobel Defence GmbH
发明人： ZHANG, Jiang , KLOFT, Peter , DELL, Klaus-Jürgen , AGOSTIN, Matthias , CORDES, Stephan , HEMMER, Axel , KÖLLER, Michael , WEISSHAUPT, Herbert , WELP, Alexandra
IPC分类号： A62C5/00 , A62C37/14 , F42C15/36
CPC分类号： A62C5/006 , A62C37/14 , F42C15/33
摘要： The invention relates to a method for thermally initiated triggering of an aerosol fire extinguisher having a strike pin (6) acted upon by an inner spring (7) and locked in the stand-by state, and after thermal initiation, the lock is removed and the strike pin (6), driven by the force of the inner spring (7), strikes against a mechanical firing cap (1), whereby an initial firing material is released in the firing cap (1), igniting a booster charge (2), the hot conversion gas thereof igniting a pyrotechnic extinguisher charge in the aerosol fire extinguisher. In order that an absolutely reliable initiation takes place under the same conditions throughout the entire service life of the aerosol fire extinguisher, it is proposed that only immediately after the thermal initiation, when the firing pin (6) is still locked, the inner spring (7) is brought to the necessary tension for triggering the firing cap (1), and only after reaching said tension is the lock of the firing pin (6) automatically released.

9. 发明公开

EP2128559A2 Initiator 失效
标题翻译：引发剂
公开(公告)号：EP2128559A2
公开(公告)日：2009-12-02
申请号：EP09002559.4
申请日：2009-02-24
申请人： Bayern-Chemie Gesellschaft für flugchemische Antriebe mbH
发明人： Naumann, Karl Wieland, Dr.
IPC分类号： F42C15/36 , F42B39/14
CPC分类号： F42C15/36 , F42B39/14
摘要： Ein Initiator (1), der bei Erreichen einer Schwelltemperatur ausgelöst wird, um die Wirkung der Entzündung eines Festtreibstoffes (12) eines Feststoffraketenmotors über der Schwelltemperatur herabzusetzen, weist eine Druckkammer (3) oder dergleichen Druckeinrichtung auf, deren Druck bei Erreichen der Schwelltemperatur in Bewegungsenergie zur Auslösung des Initiators (1) umgewandelt wird.
摘要翻译：引发剂（1）具有用于提供压力的压力单元，当达到用于释放引发剂的阈值温度时，其被转化为动能。压力单元由压力室（3）形成，压力室由闭合件封闭。压力单元包含活性介质（4），其是表现出用于打开封闭件的蒸气压的材料。封闭件由剪切片（6）形成，压力单元由预应力弹簧形成。双金属元件在达到阈值温度时释放弹簧。

10. 发明公开

EP1930541A2 Thermally activated well perforating safety system 审中-公开
标题翻译：热激活井射孔安全系统
公开(公告)号：EP1930541A2
公开(公告)日：2008-06-11
申请号：EP07254713.6
申请日：2007-12-05
申请人： HALLIBURTON ENERGY SERVICES, INC.
发明人： Grattan, Antony F. , Burleson, John D. , George, Flint R. , Hales, John H. , Harrison, Ryan A.
IPC分类号： E21B43/1185 , F42C15/34 , F42C15/36 , F42C15/44
CPC分类号： E21B43/1185 , F42C15/005 , F42C15/34 , F42C15/36 , F42C15/44
摘要： An explosives safety system (30,32) includes an explosive component (46), a blocking member (54) displaceable to selectively permit and prevent detonation of the explosive component, and a thermal actuator (56) responsive to temperature change and configured to displace the member in response to the temperature change. Another explosives safety system includes a thermal actuator with a material having a volume variable in response to the temperature change, and detonation of the explosive component being selectively permitted and prevented by the actuator when the material volume changes. A method of preventing undesired detonation of an explosive component includes the steps of: providing a material having a volume variable in response to a change in a temperature; positioning the material and the explosive component in a well, thereby increasing the material temperature; increasing the material volume in response to the increasing temperature; and permitting detonation of the explosive component in response to the increasing volume.
摘要翻译：一种爆炸物安全系统（30,32）包括一个炸药部件（46），一个可移动的选择性地允许和防止炸药部件爆炸的阻塞部件（54），以及一个响应温度变化并被配置成可以移动的热致动器（56）该成员响应温度变化。另一种爆炸物安全系统包括一个带有材料的热致动器，该材料的体积响应于温度变化而变化，并且当材料体积变化时，致动器选择性地允许和防止爆炸部件的爆炸。一种防止炸药部件不期望爆炸的方法包括以下步骤：提供具有可根据温度变化而变化的体积的材料; 将材料和炸药部件定位在井中，从而增加材料温度; 响应于温度升高而增加材料体积; 并且响应于增加的体积而允许炸药组分爆炸。

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