GB2478301A - Trigger mechanism for detecting intrusion into a secure area - Google Patents
Trigger mechanism for detecting intrusion into a secure area Download PDFInfo
- Publication number
- GB2478301A GB2478301A GB1003449A GB201003449A GB2478301A GB 2478301 A GB2478301 A GB 2478301A GB 1003449 A GB1003449 A GB 1003449A GB 201003449 A GB201003449 A GB 201003449A GB 2478301 A GB2478301 A GB 2478301A
- Authority
- GB
- United Kingdom
- Prior art keywords
- trigger mechanism
- bifilar wire
- wire
- mechanism according
- bifilar
- 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.)
- Withdrawn
Links
- 239000012212 insulator Substances 0.000 claims abstract description 8
- 238000000034 method Methods 0.000 claims description 19
- 238000009413 insulation Methods 0.000 claims description 12
- 238000012544 monitoring process Methods 0.000 claims description 9
- 229910052751 metal Inorganic materials 0.000 claims description 5
- 239000002184 metal Substances 0.000 claims description 5
- 150000002739 metals Chemical class 0.000 claims description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 230000003213 activating effect Effects 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 claims description 3
- 239000002966 varnish Substances 0.000 claims description 3
- 229920001800 Shellac Polymers 0.000 claims description 2
- 229920002635 polyurethane Polymers 0.000 claims description 2
- 239000004814 polyurethane Substances 0.000 claims description 2
- ZLGIYFNHBLSMPS-ATJNOEHPSA-N shellac Chemical compound OCCCCCC(O)C(O)CCCCCCCC(O)=O.C1C23[C@H](C(O)=O)CCC2[C@](C)(CO)[C@@H]1C(C(O)=O)=C[C@@H]3O ZLGIYFNHBLSMPS-ATJNOEHPSA-N 0.000 claims description 2
- 229940113147 shellac Drugs 0.000 claims description 2
- 235000013874 shellac Nutrition 0.000 claims description 2
- 239000004208 shellac Substances 0.000 claims description 2
- 230000003068 static effect Effects 0.000 claims description 2
- 230000001960 triggered effect Effects 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 6
- 230000004913 activation Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 238000001514 detection method Methods 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 239000000654 additive Substances 0.000 description 1
- 150000001875 compounds Chemical group 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000012858 resilient material Substances 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 239000000126 substance Chemical group 0.000 description 1
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B13/00—Burglar, theft or intruder alarms
- G08B13/02—Mechanical actuation
- G08B13/12—Mechanical actuation by the breaking or disturbance of stretched cords or wires
- G08B13/122—Mechanical actuation by the breaking or disturbance of stretched cords or wires for a perimeter fence
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B13/00—Burglar, theft or intruder alarms
- G08B13/22—Electrical actuation
- G08B13/24—Electrical actuation by interference with electromagnetic field distribution
- G08B13/2491—Intrusion detection systems, i.e. where the body of an intruder causes the interference with the electromagnetic field
- G08B13/2497—Intrusion detection systems, i.e. where the body of an intruder causes the interference with the electromagnetic field using transmission lines, e.g. cable
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Short-Circuits, Discontinuities, Leakage, Or Incorrect Line Connections (AREA)
Abstract
A trigger mechanism is disclosed comprising sensing electronics, a power source, and a length of bifilar wire. The bifilar wire has two electrically conductive filaments separated by an insulator, with a first end in electrical connection with the sensing electronics, and the power source, and a second end which is free. A circuit can be created by fusing together the two filaments in a section of the bifilar wire. The sensing electronics are configured to monitor the status of a circuit created between the bifilar wire, sensing electronics, and power source, and output a signal when the circuit is broken. On breakage of the circuit, a signal may be transmitted to one or more paging receivers, the paging receivers outputting an alarm to alert an operator that the trigger mechanism has been triggered. The bifilar wire may be used as a trip wire in a trigger mechanism for detecting intrusion into a secure area wherein the trigger mechanism may be activated by the wire being trodden on or otherwise broken by an intruder.
Description
Trigger mechanism The present invention relates to a trigger mechanism, in particular for detecting intrusion into a secure area.
It is desirable in both military and civilian settings to protect boundaries. In particular, it is desirable for security to be notified when intruders cross boundaries. For example, intruder detection is important in a military "safe zone" or to detect gate crashers in events such as music festivals and open air concerts.
One type of trigger mechanism used in military applications uses a trip wire under tension. Release of the tension in the trip wire causes activation in the trigger mechanism, for example by pulling out a pin in the mechanism. A disadvantage of this known type of trigger mechanism is that the use of trip wire under tension enables detection.
A first aspect of the present invention provides a trigger mechanism comprising: sensing electronics; a power source; a length of bifilar wire comprising two electrically conductive filaments separated by an insulator, the bifilar wire having a first end in electrical connection with the sensing electronics and the power source and a second end which is free; wherein the sensing electronics are configured to monitor the status of a circuit created between the bifilar wire, sensing electronics and power source when two filaments of the bifilar wire are fused or joined together at a section along the length of the bifilar wire.
This arrangement allows an electrical circuit to be created with a linear wire.
The bifilar wire may be wound in a coil. The two filaments in the bifilar wire may comprise metallic filaments. The two filaments may comprise either similar or dissimilar metals.
At least one filament of the bifilar wire may comprise copper.
The two filaments may be capable of being fused together by direct heat, such as a soldering iron or blow torch.In one embodiment the two filaments of the bifilar wire are capable of being fused together by a naked flame, for example a match or lighter.
Alternatively, the two filaments may be capable of being joined together by mechanical means, for example by an insulation displacement connection (IDC) The two filaments may be separated by insulation. The insulation may comprise vaporisable insulation. Examples of suitable insulation include shellac, polyurethane or other insulating varnish. In the case where the two filaments are to be joined by an insulation displacement connection, there is no advantage in using a vaporizable insulation.
A fine gauge length of bifilar wire is used, although the gauge of wire selected will depend on what the trigger mechanism is being used to detect, for example detection of unauthorised personnel or vehicles will require different gauge wires. The bifilar wire may have a gauge of 3Oswg or above. The bifilar wire may have a gauge of 30-5Oswg. In one embodiment, the bifilar wire has a gauge of 47swg. The bifilar wire may have a length of at least 1km.
The trigger mechanism may further comprise a transmitter for transmitting a signal on breakage of the circuit between the bifilar wire, sensing electronics and power source.
The trigger mechanism may further comprise a housing, wherein the housing houses the power source and sensing electronics. The housing may house a spool for the bifilar wire. An electrical connection between the spool and housing may be provided. The electrical connection may comprise a plug and socket connection.
The sensing electronics are configured to monitor the status of a circuit created between the bifilar wire, sensing electronics and power source where the two filaments of the bifilar wire are fused or joined together at a section along the length of the bifilar wire. The sensing electronics may be configured to monitor for an open circuit condition. This is suitable if the bifilar wire comprises two similar metals. Alternatively, the sensing electronics may be configured to monitor for absence of voltage. This is suitable if the bifilar wire comprises two filaments of dissimilar metals, creating a thermocouple voltage.
A second aspect of the invention provides a trigger system, comprising the trigger mechanism above and at least one receiver.
The at least one receiver may comprise an alarm which is activated on the receiver receiving a signal. The alarm may be silent. The at least one receiver may comprise at least one pager.
Alternatively, a trigger system may comprise the trigger mechanism above comprising an integral alarm.
A third aspect of the present invention provides a method of activating a trigger mechanism comprising sensing electronics, a power source and a length of bifilar wire comprising two electrically conductive filaments separated by an insulator, the bifilar wire having a first end in electrical connection with the sensing circuitry and a second end which is free, the method comprising the steps of: laying the bifilar wire in a desired location; and fusing together two filaments of the bifilar wire to create a circuit between the bifilar wire, sensing electronics and power source.
The method may further comprise the step of heating a section of the bifilar wire to fuse together the two filaments. The section of bifilar wire may be heated using a naked flame.
The step of laying the bifilar wire in a desired location may comprise unwinding it from a coil.
The method further may further comprise the step of monitoring the status of the circuit created between the bifilar wire, sensing electronics and power source. The method of monitoring the status of the circuit may comprise monitoring for an open circuit condition or an absence of voltage.
The method may further comprise the step of transmitting a signal on breakage of the circuit.
A fourth aspect of the present invention provides a use of a bifilar wire comprising two electrically conductive filaments separated by an insulator as a trip wire in a trigger mechanism.
The trigger mechanism may comprise sensing electronics and a power source in electrical connection with one end of the trip wire.
Preferred features of the second, third and fourth aspects of the invention may be as described above in connection with the first aspect.
Throughout the description and claims of this specification, the words "comprise" and "contain" and variations of the words, for example "comprising" and "comprises", mean "including but not limited to", and do not exclude other moieties, additives, components, integers or steps.
Throughout the description and claims of this specification, the singular encompasses the plural unless the context otherwise requires. In particular, where the indefinite article is used, the specification is to be understood as contemplating plurality as well as singularity, unless the context requires otherwise.
Other features of the present invention will become apparent from the following example. Generally speaking the invention extends to any novel one, or any novel combination, of the features disclosed in this specification (including any accompanying claims and drawings) . Thus features, integers, characteristics, compounds, chemical moieties or groups described in conjunction with a particular aspect, embodiment or example of the invention are to be understood to be applicable to any other aspect, embodiment or example described herein unless incompatible therewith.
Moreover unless stated otherwise, any feature disclosed herein may be replaced by an alternative feature serving the same or a similar purpose.
The present invention will now be described by way of example only and with reference to the accompanying illustrative drawings, in which: Figure 1 is a diagrammatic side view of an embodiment of the invention; Figure 2 is a schematic diagram showing the components housed within the trigger mechanism of Figure 1; Figure 3 is a flow diagram showing the set-up procedure of the trigger mechanism; Figure 4 is a flow diagram showing the sequence events which takes place following breakage of the bifilar wire in the trigger mechanism.
Figure 1 is a diagrammatic side view of an embodiment of the invention. The trigger mechanism 10 comprises a housing 12 which houses a coil of bifilar wire, a power source, sensing electronics and a transmitter. Figure 1 also shows a receiver device 14, in this case a pager, which is capable of receiving a signal transmitted from the transmitter.
A length of bifilar wire 16 can be drawn out from the coil and some is shown extending from the housing 12 in Figure 1. This wire comprises two filaments separated by an insulator. One end of the bifilar wire is in electrical connection with the sensing electronics and power supply within the housing, whilst the other end is free and can be drawn out from the housing.
Figure 2 is a schematic diagram illustrating the components of the trigger mechanism which are housed within the housing. The components comprise a spool 18, which contains the coil of bifilar wire, which may exceed 1km in length. A length of bifilar wire 16 is shown extending from the spool 18. Storing the coil of bifilar wire inside the spool has the benefit of eliminating rotation of the spool on drawing out of the wire.
The spool 18 is connected to a printed circuit board (PCB) 20 which comprises sensing electronics 24and a transmitter 22. Also within the housing and connected to the PCB are batteries 26, an activation switch 28, an LED 30, a test switch 32 and an aerial 34.
The spool 18 is electrically connected to the electronics in the housing via an electrical connection 36, comprising a plug and socket. In this embodiment, the spool is provided with an electrical socket, with the corresponding plug being mounted in the housing, although the opposite configuration is also possible. A length of bifilar wire is wound within the spool and one end is attached to the electrical connection 36. The electrical connection between the spoo1 and housing is fully polarised, preventing the connection from being made the wrong way. The spool has a narrow neck 38, through which the free end of bifilar wire extends. This narrow neck is plugged with a foam or other resilient material, to prevent the wire from falling out of the spool and to maintain adequate friction when the free end of the wire is pulled.
The outer end of the coil of the bifilar wire is static and attached to electrical connection 36, whilst the inner end of the coil is free and extends through the neck 38 of the spool, enabling it to be pulled freely. This arrangement allows rapid deployment of the bifilar wire without tangling.
The trigger mechanism is set up as illustrated in the flow diagram of Figure 3. The free end of the bifilar wire is drawn out from the coil and laid out as desired, for example along a boundary 40. Once a sufficient length of bifilar wire has been unravelled and arranged as desired, a section of the bifilar wire is fused 42. This section is preferably at or close to the free end of the length of bifilar wire. The section of wire is fused, for example by heating with a naked flame, such as a match or lighter. This causes the two individual filaments of the bifilar wire to fuse together, creating a circuit between the bifilar wire, sensing electronics and power source. The trigger mechanism is then switched on 44, using the activation switch. The activation switch allows the trigger mechanism to be turned on but does not provide an option for it to be switched off. The status of the trigger mechanism is checked 46 by monitoring the status LED. The status LED will illuminate for a set period of time, for example 30 seconds, in response to the activation switch being switched on. The LED is a bicolour LED with shows a first colour for system activated and a second colour for system failure. Finally, the transmitter will transmit a signal to the receiver 38 to confirm that the trigger mechanism is activated.
At any time, the status of the trigger mechanism can be checked by pressing the test switch; this will cause the status LED to light up for a set period of time, showing the status of the trigger mechanism.
Once the trigger mechanism has been set up and activated, any damage to the bifilar wire will result in the circuit being broken. Figure 4 is a flow diagram illustrating the sequence of events which follows the breakage of the bifilar wire. The trigger mechanism is activated by a break in the bifilar wire 50. This can be caused by the wire being trodden on or otherwise broken by an intruder and causes the circuit to be broken. A break in the circuit is detected by sensing electronics 52 which monitors the status of the circuit. On breakage of the circuit, the sensing electronics will cause the transmitter to transmit a signal 54. This transmitted signal is received by one or more receivers 56. The receivers may comprise pagers or other suitable devices, such as mobile telephones. The one or more receivers output an alarm 58 to alert the operator that the trigger mechanism has been triggered. The alarm may be silent, for example a vibration.
The bifilar wire is very fine, in this embodiment 47 swg (standard wire gauge), which allows it to be easily hidden from view. This low visibility is further enhanced by using a dark colour, such as green or black. Additionally, the bifilar wire has a matt finish, which enhances the low visibility. The use of a very fine wire not only allows the wire to be easily hidden but also causes it to break very easily. The low breaking strain has the advantage that the wire is not required to be kept under tension, making detection extremely difficult. Furthermore, such a fine wire enables a light weight device to be produced. In different application, use of a thicker wire may be desired, for example to detect vehicles, such as tanks, crossing a boundary.
The bifilar wire used in this embodiment has two copper filaments separated by insulating varnish. The combination of a very fine wire, the use of a material for the filaments with a low melting point and a vaporisable insulation ensures that the filaments can easily be fused together with a naked flame.
The trigger mechanism of the present invention has the advantage of being light weight, low visibility and capable of rapid deployment. The fact that the bifilar wire is not required to be under tension makes it especially difficult to detect. The trigger mechanism is very versatile and can be deployed over ground, buried or submersed.
Claims (39)
- Claims 1. A trigger mechanism comprising: sensing electronics; a power source; a length of bifilar wire comprisThg two electrically conductive filaments separated by an insulator, the bifilar wire having a first end in electrical connection with the sensing electronics and the power source and a second end which is free; wherein the sensing electronics are configured to monitor the status of a circuit created between the bifilar wire, sensing electronics and power source when two filaments of the bifilar wire are fused or joined together at a section along the length of the bifilar wire.
- 2. A trigger mechanism according to claim 1, wherein the bifilar wire is wound in a coil.
- 3. A trigger mechanism according to any one of the preceding claims wherein the two filaments in the bifilar wire comprise metallic filaments.
- 4. A trigger mechanism according to claim 3, wherein the two filaments comprise similar metals.
- 5. A trigger mechanism according to claim 3 wherein the two filaments comprise dissimilar metals.
- 6. A trigger mechanism according to any one of claims 1 to 4, wherein at least one filament of the bifilar wire comprise copper.
- 7. A trigger mechanism according to any one of the preceding claims, wherein the two filaments of the bifilar wire are capable of being fused together by a direct heat source.
- 8. A trigger mechanism according to claim 7, wherein the direct heat source comprises a naked flame.
- 9. A trigger mechanism according to any one of claims 1 to 6 wherein the two filaments of the bifilar wire are capable of being joined together by mechanical means.
- 10. A trigger mechanism according to any one of the preceding claims, wherein the two filaments are separated by insulation.
- 11. A trigger mechanism according to claim 10 wherein the insulation comprises vaporisable insulation.
- 12. A trigger mechanism according to any one of claims 10 or 11, wherein the insulation comprises shellac, polyurethane or other insulating varnish.
- 13. A trigger mechanism according to any one of the preceding claims, wherein the bifilar wire has a gauge of loswg or above.
- 14. A trigger mechanism according to any one of the preceding claims, wherein the bifilar wire has a gauge of 3oswg or above.
- 15. A trigger mechanism according to any one of the preceding claims, wherein the bifilar wire has a gauge of 30-5oswg.
- 16. A trigger mechanism according to any one of the preceding claims, wherein the bifilar wire has a gauge of 47swg.
- 17. A trigger mechanism according to any one of the preceding claims, wherein the bifilar wire has a length of at least 1km.
- 18. A trigger mechanism according to any one of the preceding claims, further comprising a transmitter for transmitting a signal on breakage of the circuit between the bifilar wire, sensing electronics and power source.
- 19. A trigger mechanism according to any one of the preceding claims, further comprising a housing, wherein the housing houses the power source and sensing electronics.
- 20. A trigger mechanism according to claim 19, wherein the housing further houses a spooi for the bifilar wire.
- 21. A trigger mechanism according to claim 20, comprising an electrical connection between the spooi and housing.
- 22. A trigger mechanism according to claim 21, wherein the electrical connection comprises a plug and socket connection.
- 23. A trigger mechanism according to any one of the preceding claims wherein the bifilar wire is stored in a coil and wherein the outer end is static and the inner end is free.
- 24. A trigger system, comprising the trigger mechanism of any of claims 1 to 23 and at least one receiver.
- 25. A trigger system according to claim 24, wherein the at least one receiver comprises an alarm which is activated on the receiver receiving a signal.
- 26. A trigger system according to claim 25 wherein the alarm is silent.
- 27. A trigger system according to any one of claims 23 to 26, wherein the at least one receiver comprises at least one pager.
- 28. A method of activating a trigger mechanism comprising sensing electronics, a power source and a length of bifilar wire comprising two electrically conductive filaments separated by an insulator, the bifilar wire having a first end in electrical connection with the sensing circuitry and a second end which is free, the method comprising the steps of: laying the bifilar wire in a desired location; and fusing or joining together two filaments of the bifilar wire to create a circuit between the bifilar wire, sensing electronics and power source.
- 29. A method according to claim 28, comprising the step of heating a section of the bifilar wire to fuse together the two filaments.
- 30. A method according to claim 29, wherein the section of bifilar wire is heated using a naked flame.
- 31. A method according to any one of claims 28 to 30, wherein the step of laying the bifilar wire in a desired location comprises unwinding it from a coil.
- 32. A method according to any one of claim 28 to 31, wherein the method further comprises the step of monitoring the status of the circuit created between the bifilar wire, sensing electronics and power source.
- 33. A method according to claim 32, wherein the step of monitoring the status of the circuit comprises monitoring for an open circuit condition.
- 34. A method according to claim 32, wherein the step of monitoring the status of the circuit comprises monitoring for absence of voltage.
- 35. A method according to any one of claims 28 to 34, wherein the method further comprises the step of transmitting a signal on breakage of the circuit.
- 36. Use of a bifilar wire comprising two electrically conductive filaments separated by an insulator as a trip wire in a trigger mechanism.
- 37. Use of a bifilar wire in a trip wire according to claim 36 wherein the trigger mechanism comprises sensing electronics and a power source in electrical connection with one end of the trip wire.
- 38. A trigger mechanism substantially as herein described, with reference to the accompanying illustrative drawings.
- 39. A method of activating a trigger mechanism substantially as herein described, with reference to the accompanying illustrative drawings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1003449A GB2478301A (en) | 2010-03-02 | 2010-03-02 | Trigger mechanism for detecting intrusion into a secure area |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1003449A GB2478301A (en) | 2010-03-02 | 2010-03-02 | Trigger mechanism for detecting intrusion into a secure area |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB201003449D0 GB201003449D0 (en) | 2010-04-14 |
| GB2478301A true GB2478301A (en) | 2011-09-07 |
| GB2478301A8 GB2478301A8 (en) | 2011-11-09 |
Family
ID=42125837
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1003449A Withdrawn GB2478301A (en) | 2010-03-02 | 2010-03-02 | Trigger mechanism for detecting intrusion into a secure area |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2478301A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3867564A (en) * | 1973-06-19 | 1975-02-18 | Honeywell Inc | Dual wire intruder detector |
| DE1910780A1 (en) * | 1968-03-01 | 1976-09-02 | France Etat | Electrical initiation device for antipersonnel mines - has battery and bifilar flexible triggering cable connected to thyristor |
| DE1967221B1 (en) * | 1968-03-01 | 1980-09-11 | L'etat Francais Represente Par Le Delegue General Pour L'armement, Paris | Safety and control device on electric mine detonators |
| DE3338936A1 (en) * | 1983-10-27 | 1985-05-09 | Diehl GmbH & Co, 8500 Nürnberg | Detonating device for a defensive mine |
| US4887069A (en) * | 1986-11-06 | 1989-12-12 | Control Data Canada Limited | Perimeter intrusion detection system with block ranging capabilities |
| US5247270A (en) * | 1987-12-01 | 1993-09-21 | Senstar Corporation | Dual leaky cables |
| US5473336A (en) * | 1992-10-08 | 1995-12-05 | Auratek Security Inc. | Cable for use as a distributed antenna |
| US5705984A (en) * | 1996-05-10 | 1998-01-06 | The United States Of America As Represented By The Secretary Of The Navy | Passive intrusion detection system |
-
2010
- 2010-03-02 GB GB1003449A patent/GB2478301A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1910780A1 (en) * | 1968-03-01 | 1976-09-02 | France Etat | Electrical initiation device for antipersonnel mines - has battery and bifilar flexible triggering cable connected to thyristor |
| DE1967221B1 (en) * | 1968-03-01 | 1980-09-11 | L'etat Francais Represente Par Le Delegue General Pour L'armement, Paris | Safety and control device on electric mine detonators |
| US3867564A (en) * | 1973-06-19 | 1975-02-18 | Honeywell Inc | Dual wire intruder detector |
| DE3338936A1 (en) * | 1983-10-27 | 1985-05-09 | Diehl GmbH & Co, 8500 Nürnberg | Detonating device for a defensive mine |
| US4887069A (en) * | 1986-11-06 | 1989-12-12 | Control Data Canada Limited | Perimeter intrusion detection system with block ranging capabilities |
| US5247270A (en) * | 1987-12-01 | 1993-09-21 | Senstar Corporation | Dual leaky cables |
| US5473336A (en) * | 1992-10-08 | 1995-12-05 | Auratek Security Inc. | Cable for use as a distributed antenna |
| US5705984A (en) * | 1996-05-10 | 1998-01-06 | The United States Of America As Represented By The Secretary Of The Navy | Passive intrusion detection system |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2478301A8 (en) | 2011-11-09 |
| GB201003449D0 (en) | 2010-04-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |