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1. 发明专利

JPS60176000A METHOD AND DEVICE FOR TRIGGERING ELECTRONIC SHORT-DELAY BLASTING DETONATOR WHILE FORMING TIME DIFFERENCE 失效
公开(公告)号：JPS60176000A
公开(公告)日：1985-09-10
申请号：JP26868984
申请日：1984-12-21
申请人： DYNAMIT NOBEL AG
发明人： YOHAN FURORIN , FURIIDORITSUHI HAINEMAIAA , PEETAA REE , HANSU MARUTEIN SHIYUTERURE
IPC分类号： F42D1/04 , F24D1/04 , F24D1/06 , F42B3/10 , F42B3/16 , F42C20060101 , F42D1/045 , F42D1/055 , F42D1/06

2. 发明专利

JPH03502599A 失效
公开(公告)号：JPH03502599A
公开(公告)日：1991-06-13
申请号：JP50868989
申请日：1989-08-14
IPC分类号： F42B20060101 , F42C20060101 , F42C1/00 , F42C1/04 , F42C15/00 , F42C15/24
摘要： PCT No. PCT/DE89/00533 Sec. 371 Date Apr. 13, 1990 Sec. 102(e) Date Apr. 13, 1990 PCT Filed Aug. 14, 1989 PCT Pub. No. WO90/02309 PCT Pub. Date Mar. 8, 1990.The invention relates to an impact fuse (2) having fore-bore safety for a projectile (1), comprising a percussion needle (3) stationary on the fuse and an impact body (4) containing a percussion cap (5) and supported slidingly in the direction of flight, as well as a race for a blocking ball (23) between the impact body and the inner wall of the projectile casing. Which, upon premature impact on an obstacle, is jammed in its race (22) between a shoulder (18, 19, 20) on the inner wall of the casing and a ramp (17) of a groove (14, 15, 16) on the impact body (4), thereby preventing detonation. In order to allow for adjustment of predefined distances for the fore-bore safety, the invention proposes giving the race (22) for the blocking ball (23) a stepped design so that the blocking ball (23) can be jammed at several places within the fuse (2) between shoulders (18, 19, 20) and ramps (17) of different grooves (14, 15, 16).

3. 发明专利

JPS5773400A Safety device for spiral lead detonator 失效
标题翻译：用于螺旋引爆装置的安全装置
公开(公告)号：JPS5773400A
公开(公告)日：1982-05-08
申请号：JP13342481
申请日：1981-08-27
申请人： Oerlikon Buehrle Holding Ag
发明人： ROOBERUTO APOTOHEROTSU
IPC分类号： F42C15/16 , F42C20060101 , F42C15/20 , F42C15/24 , F42C15/26

4. 发明专利

JP2552924B2 失效
公开(公告)号：JP2552924B2
公开(公告)日：1996-11-13
申请号：JP50868989
申请日：1989-08-14
申请人： NIKO PIROTEHINIIKU HANSU YURUGEN DEIIDERITSUHISU KG
发明人： RYUTSUBERUSU UIRURI
IPC分类号： F42B20060101 , F42C20060101 , F42C1/00 , F42C1/04 , F42C15/00 , F42C15/24
摘要： PCT No. PCT/DE89/00533 Sec. 371 Date Apr. 13, 1990 Sec. 102(e) Date Apr. 13, 1990 PCT Filed Aug. 14, 1989 PCT Pub. No. WO90/02309 PCT Pub. Date Mar. 8, 1990.The invention relates to an impact fuse (2) having fore-bore safety for a projectile (1), comprising a percussion needle (3) stationary on the fuse and an impact body (4) containing a percussion cap (5) and supported slidingly in the direction of flight, as well as a race for a blocking ball (23) between the impact body and the inner wall of the projectile casing. Which, upon premature impact on an obstacle, is jammed in its race (22) between a shoulder (18, 19, 20) on the inner wall of the casing and a ramp (17) of a groove (14, 15, 16) on the impact body (4), thereby preventing detonation. In order to allow for adjustment of predefined distances for the fore-bore safety, the invention proposes giving the race (22) for the blocking ball (23) a stepped design so that the blocking ball (23) can be jammed at several places within the fuse (2) between shoulders (18, 19, 20) and ramps (17) of different grooves (14, 15, 16).

5. 发明专利

JPH0814475B2 失效
公开(公告)号：JPH0814475B2
公开(公告)日：1996-02-14
申请号：JP50328586
申请日：1985-12-09
IPC分类号： F42B20060101 , F42B5/02 , F42B5/285 , F42B5/307 , F42C20060101

6. 发明专利

JPS62259000A DELAYED BLASTING DETONATOR 失效
公开(公告)号：JPS62259000A
公开(公告)日：1987-11-11
申请号：JP10018987
申请日：1987-04-24
申请人： DYNAMIT NOBEL AG
发明人： HANSU FUROORIN
IPC分类号： F42B3/16 , F42B20060101 , F42C20060101

7. 发明专利

JPS6137560B2 失效
公开(公告)号：JPS6137560B2
公开(公告)日：1986-08-25
申请号：JP13342481
申请日：1981-08-27
申请人： UERUKUTSUOIKU MAS FAB EERIKON BYUURE AG
发明人： ROOBERUTO AHOTOHEROTSU
IPC分类号： F42C15/16 , F42C20060101 , F42C15/20 , F42C15/24 , F42C15/26

8. 发明授权

US5090321A Detonator actuator 失效
标题翻译：雷管执行器
公开(公告)号：US5090321A
公开(公告)日：1992-02-25
申请号：US269117
申请日：1988-11-09
申请人： David M. Abouav
发明人： David M. Abouav
IPC分类号： F42B3/12 , F42C20060101 , F42C15/40 , F42D1/05 , F42D1/055
CPC分类号： F42B3/122 , F42C15/40 , F42D1/055
摘要： An actuator for use in conjunction with a detonator for blasting comprises electronic circuitry which on receiving input signals generates an output arm signal to arm a detonator, and then after a predetermined delay an output actuate signal to fire the detonator and an associated explosive charge. The delay is capable of being remotely and precisely set. The actuator is preferably used in conjunction with a control device which has a microcomputer whose memory contains arm and actuate codes and which has both arm and actuate keys. This microcomputer is such that the actuate key must be operated within a predetermined period after operation of the arm key, otherwise an actuate signal is not transmitted to the actuator.
摘要翻译：用于与用于爆破的雷管结合使用的致动器包括电子电路，其在接收到输入信号时产生输出臂信号以布置雷管，然后在预定延迟之后输出致动信号以引爆雷管和相关联的炸药。延迟能够远程和精确地设置。致动器优选地与具有其存储器包含臂和致动代码并具有臂和致动键的微型计算机的控制装置结合使用。该微型计算机使得在手臂键操作之后的预定时间内必须操作致动键，否则致动信号不会传递到致动器。

9. 发明授权

US3850387A Deflection device for rocket motor propelled projectiles 失效
标题翻译：用于摇臂电机螺旋桨的偏转装置
公开(公告)号：US3850387A
公开(公告)日：1974-11-26
申请号：US37966173
申请日：1973-07-16
申请人： BOFORS AB
发明人： BJORNSON B , STRADALEN Y
IPC分类号： F42B10/66 , F42B20060101 , F42C20060101 , F42B13/30
CPC分类号： F42B10/665
摘要： A rocket propelled projectile is provided with a deflection device for temporarily deflecting the direction of flow of a gas jet issuing from the nozzle of the rocket motor. The deflection device comprises a flow deflecting member which is pivotally attached to the rocket motor and which extends to an active position wherein the flow deflecting member overlies a portion of the exhaust area of the nozzle. The deflecting member is temporarily retained in its active position by a locking pin which is positioned within the nozzle in the path of flow of the gas jet. The locking pin is eroded by the gas jet to release the flow deflecting member after a period of time, to permit the flow deflecting member to pivot to an inactive position wherein the flow deflecting member no longer overlies the exhaust area of the nozzle.
摘要翻译：火箭推进射弹设置有用于暂时偏转从火箭发动机的喷嘴发出的气体射流的流动方向的偏转装置。偏转装置包括流动偏转构件，其可枢转地附接到火箭发动机并且延伸到活动位置，其中流动偏转构件覆盖在喷嘴的排气区域的一部分上。偏转构件通过在气体射流的流动路径中位于喷嘴内的锁定销暂时保持在其主动位置。锁定销被气体喷射器侵蚀以在一段时间之后释放流动偏转构件，以允许流动偏转构件枢转到非活动位置，其中流动偏转构件不再覆盖喷嘴的排气区域。

10. 发明专利

JPH0942897A ELECTRONIC TYPE DELAY DETONATOR 失效
公开(公告)号：JPH0942897A
公开(公告)日：1997-02-14
申请号：JP19061595
申请日：1995-07-26
申请人： ASAHI CHEMICAL IND
发明人： KUROKI KAZUHIRO , SAKAMOTO MIDORI
IPC分类号： F42B3/12 , F42B20060101 , F42B3/16 , F42C20060101
摘要： PROBLEM TO BE SOLVED: To provide an electronic type delay detonator having a high anti-shock characteristic against an explosion in which a plurality of explosives are loaded in an item to be broken and an explosion delay tinme is controlled in a high accurate manner during an explosion work for exploding these explosives in sequence. SOLUTION: There are provided an energy accumulation circuit 5 for accumulating electrical energy supplied from a blasting device, a first oscillator circuit 11 with a crystal oscillator element operated by the electrical energy accumulated in the energy accumulating circuit being applied as a reference value, a second oscillator circuit 13 having an anti-shock characteristic, and a time counting period making circuit 14 for use in making a time counting period by the second oscillator circuit in such a way that the time counting period may coincide with a reference period made by the first oscillator circuit. This electronic type delay detonator is also comprised of trigger signal generating circuits 31, 32 for outputting a trigger signal in reference to the time counting period under an operation of the second oscillator circuit and of an electrical discharging circuit 8 for discharging electrical energy responding against the trigger signal and accumulated in the energy accumulating circuit.

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