发明名称 SHOCK TUBE INITIATOR
摘要 <p>A shock tube initiator (STI) for allowing the remote and/or manual initiation of at least one shock tube, typically two shock tubes is disclosed. The STI consists of: a) at least one coupling 8, connected to a shock tube containing a shot shell primer that upon firing initiates burning of the shock tube,b) a cockable mechanical firing mechanism 7 adjacent to the coupling 8 wherein the mechanical firing mechanism 7 is adapted to strike respective firing pins 9 within the couplings,c) a safety mechanism 15 adapted to allow the mechanical firing mechanism 7 to ignite said explosive charge only when the safety mechanism 15 is moved from a safe mode position to an armed position,d) a rotary solenoid valve 24, electrically connected to and energised by a remote controlled operating system, ande) an actuator 10 positioned between and engageable with the rotary electro-mechanical energising means 24 and the firing mechanism 7 and wherein said actuator 10 is adapted to be actuated either by the rotarysolenoid valve 24 , when energised, or manually manipulated (13) to allow the cockable mechanical firing mechanism 7 when cocked, to ignite said shell primer.</p>
申请公布号 WO2005054073(A1) 申请公布日期 2005.06.16
申请号 WO2003NZ00264 申请日期 2003.12.01
申请人 MARINE AIR SYSTEMS (NZ) LTD;BALLANTINE, ROGER;HORNBROOK, ANTHONY, PAUL;MOORE, IAN;HAMILTON, DAVE, NORMAN 发明人 BALLANTINE, ROGER;HORNBROOK, ANTHONY, PAUL;MOORE, IAN;HAMILTON, DAVE, NORMAN
分类号 C06C5/04;F42B3/10;F42D1/04;(IPC1-7):B65D47/24;B65D47/26;B65D47/36;B65D41/50 主分类号 C06C5/04
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