GB1371111A - Remote detonation system - Google Patents
Remote detonation systemInfo
- Publication number
- GB1371111A GB1371111A GB4731372A GB4731372A GB1371111A GB 1371111 A GB1371111 A GB 1371111A GB 4731372 A GB4731372 A GB 4731372A GB 4731372 A GB4731372 A GB 4731372A GB 1371111 A GB1371111 A GB 1371111A
- Authority
- GB
- United Kingdom
- Prior art keywords
- detonation
- command signals
- main
- signal
- loop
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C23/00—Non-electrical signal transmission systems, e.g. optical systems
- G08C23/02—Non-electrical signal transmission systems, e.g. optical systems using infrasonic, sonic or ultrasonic waves
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Selective Calling Equipment (AREA)
- Air Bags (AREA)
Abstract
1371111 Controlling and actuating by ultrasonic waves OKI ELECTRIC INDUSTRY CO Ltd and TAISEI CORP 13 Oct 1972 [15 Oct 1971] 47313/72 Heading G4F In a system for underwater explosive detonation employing ultrasonic signals, a control station emits frequency modulated command signals which are received by respective detonation control elements each arranged to detonate a respective body of explosive by energizing ignition means via a plurality of switches at. least one of the switches being closed by means of the command signals. In a preferred embodiment the command signals are received by a main detonation control element which detonates its associated charge; each of a number of auxiliary detonation control elements receives the command signals and the shock front from detonation of the main charge and is thereby caused to detonate an associated auxiliary charge. The main control element may float near the surface of the water while the auxiliary control elements are disposed in a rock formation to be blasted (Fig. 2, not shown), or all the control elements may be disposed in the rock formation (Fig. 1, not shown). Control station (Fig. 3, not shown).-The carrier signal from an oscillator (12) is modulated (at 16) alternately by a signal f 1 from an oscillator (13) and a signal f 2 from an oscillator (14) which are connected in alternation by a timing gate circuit (15) to the modulator. The modulated signals are amplified and transmitted. The timing gate circuit (15) is described (Fig, 7, not shown) and comprises an arrangement of two timers (T 1 , T 2 ) and four relays (RL-1 to RL-4). Main detonation control element (Fig. 4, not shown).-The received command signals are demodulated (at 20) and the signals f 1 ,f 2 extracted in separate loops each including an appropriate bandpass filter (21 or 22), rectifying and integrating circuit (23 or 26) and amplifier (24 or 27). Thence, the processed signal f 1 operates a first switch (25) while the later-received processed signal f 2 operates a second switch (28) so that, with the two switches closed, a current source (29) is connected to a detonator (5). In a modification, in which a control station simultaneously transmits command signals, the main detonation control element is constructed to produce a delay so as to enable sequential closing of the two switches. To this end (Fig. 8, not shown) the output from the demodulator (20) is divided and passes, in one loop, through a filter (21), rectifying and integrating circuit (57) and Schmit trigger (59) to a first monostable multivibrator (61) whose output is connected to the first switch (25) as well as to the trigger input of a second monostable multivibrator (62) whose output forms one input to an AND-gate (64) whose output is connected to the second switch (28). The signal passes, in the other loop, through a filter (22), rectifying and integrating circuit (58) and Schmit trigger (60) to the second input of the AND-gate (64). Auxiliary detonation control element (Fig. 5, not shown). The command signals and the shock front from detonation of the main charge are received (as at 8). The command signals are processed in a first loop which may include a demodulator (32) and a bandpass filter (33) arranged to pass signal f 1 . Alternatively, the loop may comprise a mechanical or electrical timer which operates during the period of duration of the command signals. The output from the first loop is supplied to a first switch (36). The shock front signal is processed in a second loop comprising a limiter (38) which produces a pulse to close a second switch (37) so that, with both switches closed, current is supplied from a source (39) to a detonator (10). Various modifications of the main and auxiliary detonation control elements are described. An ignition circuit, for energizing a detonator upon receipt of two input signals (from the switches described) is also described (Fig. 6, not shown). In another embodiment the detonation control elements are all in the form of the described main detonation control element, the auxiliary detonation control elements being omitted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP46080970A JPS5146248B2 (en) | 1971-10-15 | 1971-10-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1371111A true GB1371111A (en) | 1974-10-23 |
Family
ID=13733356
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4731372A Expired GB1371111A (en) | 1971-10-15 | 1972-10-13 | Remote detonation system |
Country Status (7)
Country | Link |
---|---|
US (1) | US3780654A (en) |
JP (1) | JPS5146248B2 (en) |
CA (1) | CA972061A (en) |
DE (1) | DE2250630C3 (en) |
GB (1) | GB1371111A (en) |
IT (1) | IT969003B (en) |
SE (1) | SE397135B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2117948A (en) * | 1982-03-22 | 1983-10-19 | Ml Aviation Co Ltd | Initiation of devices by high- frequency sound waves |
CN110749254A (en) * | 2019-10-16 | 2020-02-04 | 中国兵器工业集团第二一四研究所苏州研发中心 | Short-delay trigger ignition circuit |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5028621B2 (en) * | 1972-06-23 | 1975-09-17 | ||
US3914732A (en) * | 1973-07-23 | 1975-10-21 | Us Energy | System for remote control of underground device |
GB1431600A (en) * | 1973-10-31 | 1976-04-07 | Ici Ltd | Method of blasting and a detenator firing device therefor |
GB1526634A (en) * | 1976-03-30 | 1978-09-27 | Tri Electronics Ab | Electric detonator cap |
DE2939700C2 (en) * | 1979-09-29 | 1983-09-08 | Rheinmetall GmbH, 4000 Düsseldorf | Safety ignition circuit for an underwater detonator |
US4382410A (en) * | 1980-12-22 | 1983-05-10 | Bowling David S | Explosive blasting method and means |
US4496010A (en) * | 1982-07-02 | 1985-01-29 | Schlumberger Technology Corporation | Single-wire selective performation system |
ATE45036T1 (en) * | 1984-09-04 | 1989-08-15 | Ici Plc | METHOD AND DEVICE FOR SAFE REMOTE CONTROLLED INITIATION OF FIRING ELEMENTS. |
US5202532A (en) * | 1990-05-21 | 1993-04-13 | Alliant Techsystems Inc. | Autonomous acoustic detonation device |
US6213021B1 (en) * | 1999-12-16 | 2001-04-10 | The United States Of America As Represented By The Secretary Of The Navy | Electromagnetic sea mine detonation system |
ATE348313T1 (en) * | 2001-10-02 | 2007-01-15 | Orica Explosives Tech Pty Ltd | REMOTE CONTROLLED IGNITION SYSTEM WITH FREQUENCY DIVERSITY |
DE102006004517A1 (en) | 2006-02-01 | 2007-08-09 | Eads Deutschland Gmbh | Method and system for defense against missiles |
PE20080595A1 (en) * | 2006-04-28 | 2008-05-17 | Orica Explosives Tech Pty Ltd | METHODS FOR CONTROLLING COMPONENTS OF BLADE APPARATUS, BLADE APPARATUS AND COMPONENTS THEREOF |
NZ549967A (en) * | 2006-09-19 | 2008-06-30 | Mas Zengrange Nz Ltd | Initiator for the remote initiation of explosive charges |
NZ579690A (en) * | 2009-09-16 | 2010-01-29 | Mas Zengrange Nz Ltd | Remote Initiator Breaching System |
US9568294B2 (en) | 2013-03-08 | 2017-02-14 | Ensign-Bickford Aerospace & Defense Company | Signal encrypted digital detonator system |
US10060716B2 (en) * | 2014-12-01 | 2018-08-28 | Matthew Creedican | Explosives manipulation using ultrasound |
CN112924800B (en) * | 2021-03-06 | 2022-08-12 | 中北大学 | Voltage continuously adjustable electric explosion foil volt-ampere characteristic testing device and charging and discharging method |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3125953A (en) * | 1964-03-24 | Amplifier | ||
US2465009A (en) * | 1945-10-11 | 1949-03-22 | Leland H Chase | Concussion detonator |
DE961958C (en) * | 1954-11-11 | 1957-04-11 | Ernst Hans Doerpinghaus Dipl I | Electric ignition device |
DE1062320B (en) * | 1955-05-07 | 1959-07-30 | Deutsche Elektronik Gmbh | Method for the wireless action on energy-consuming receivers by means of a wave train of limited duration |
-
1971
- 1971-10-15 JP JP46080970A patent/JPS5146248B2/ja not_active Expired
-
1972
- 1972-10-13 SE SE7213234A patent/SE397135B/en unknown
- 1972-10-13 GB GB4731372A patent/GB1371111A/en not_active Expired
- 1972-10-13 CA CA153,886A patent/CA972061A/en not_active Expired
- 1972-10-16 IT IT30507/72A patent/IT969003B/en active
- 1972-10-16 US US00297985A patent/US3780654A/en not_active Expired - Lifetime
- 1972-10-16 DE DE2250630A patent/DE2250630C3/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2117948A (en) * | 1982-03-22 | 1983-10-19 | Ml Aviation Co Ltd | Initiation of devices by high- frequency sound waves |
CN110749254A (en) * | 2019-10-16 | 2020-02-04 | 中国兵器工业集团第二一四研究所苏州研发中心 | Short-delay trigger ignition circuit |
CN110749254B (en) * | 2019-10-16 | 2022-04-22 | 中国兵器工业集团第二一四研究所苏州研发中心 | Short-delay trigger ignition circuit |
Also Published As
Publication number | Publication date |
---|---|
IT969003B (en) | 1974-03-30 |
JPS5146248B2 (en) | 1976-12-08 |
DE2250630C3 (en) | 1978-11-02 |
DE2250630B2 (en) | 1978-03-02 |
CA972061A (en) | 1975-07-29 |
US3780654A (en) | 1973-12-25 |
SE397135B (en) | 1977-10-17 |
DE2250630A1 (en) | 1973-05-03 |
JPS4848611A (en) | 1973-07-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |