WO2011015867A1 - Improved apparatus for delivering an electric shock - Google Patents

Improved apparatus for delivering an electric shock Download PDF

Info

Publication number
WO2011015867A1
WO2011015867A1 PCT/GB2010/051284 GB2010051284W WO2011015867A1 WO 2011015867 A1 WO2011015867 A1 WO 2011015867A1 GB 2010051284 W GB2010051284 W GB 2010051284W WO 2011015867 A1 WO2011015867 A1 WO 2011015867A1
Authority
WO
WIPO (PCT)
Prior art keywords
electrically conductive
base
conductive element
channels
conductive elements
Prior art date
Application number
PCT/GB2010/051284
Other languages
French (fr)
Inventor
Ray Ritson
Original Assignee
Pestration Limited
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Pestration Limited filed Critical Pestration Limited
Priority to US13/388,543 priority Critical patent/US20120127624A1/en
Priority to EP10742538.1A priority patent/EP2461674B1/en
Publication of WO2011015867A1 publication Critical patent/WO2011015867A1/en

Links

Classifications

    • AHUMAN NECESSITIES
    • A01AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01MCATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
    • A01M29/00Scaring or repelling devices, e.g. bird-scaring apparatus
    • A01M29/24Scaring or repelling devices, e.g. bird-scaring apparatus using electric or magnetic effects, e.g. electric shocks, magnetic fields or microwaves
    • A01M29/26Scaring or repelling devices, e.g. bird-scaring apparatus using electric or magnetic effects, e.g. electric shocks, magnetic fields or microwaves specially adapted for birds, e.g. electrified rods, cords or strips

Definitions

  • the present invention relates to an apparatus for repelling birds, and in particular to an apparatus for repelling birds capable of supporting significant weight.
  • Helicopter landing pads present a particular problem, especially those located on oil rigs, since the oil rig is likely to be the only structure within a large area upon which sea birds may land. Furthermore, they present a very harsh environment in which to operate any apparatus.
  • vermin also present problems which may be addressed by the use of apparatus for delivering an electric shock to the vermin in question.
  • apparatus for delivering an electric shock to the vermin in question may be used to deter rats from entering buildings.
  • United States Patent 6,006,698 describes an electrical bird repelling device comprising a base made of an insulating material, and one or more electrically conductive rails disposed on the base. An electric potential is applied to each of the rails such that there is a potential difference between the two rails. When a bird lands on the electrical device and bridges the two rails, current flows between the two rails and the bird is given a mild electric shock which repels the bird from the area of the electrical device.
  • the electrically conducting metal rails equipped with blades are laid in a base material formed of a polyvinyl chloride (PVC) extruded profile having a hardness of 83.
  • the base has a very low height (2.4mm) the purpose of which is to assist the device blending in with the surface from which birds are to be deterred.
  • the upstanding spikes prevent nesting on the device and are also said to create a noise that is disliked by birds.
  • DE29610206U1 describes another electric-shock device adapted to deter birds, and comprises a base upon which are mounted alternate positive and negative upstanding tracks. This device is adapted to be mounted on edges of buildings and the like to prevent birds perching thereon.
  • EPl 382243 describes an electric-shock sheet which may be laid out across a surface to be kept free of birds, or other vermin. However, such a sheet is not capable of supporting a significant weight without itself being damaged.
  • DE G 9405347 describes an electrified mat to protect against animals and adapted to be laid out across a surface, such as the floor of a garage or carport. The mat is laid out across the surface and a car may drive over it. The mat comprises a carrier layer 2 and electrified zones 3, which are isolated from each other. The car driver switches off the electrical supply to the mat to reach the vehicle parked in the garage.
  • the construction of the electrified mat in DE G 9405347 comprises a base, a plurality of exposed live wires extending one way across the carrier layer and a plurality of spaced apart clips extending normal to the direction of the live wires and holding them in place.
  • an electric shock delivery apparatus comprising a base of an electrically insulating material, the base having formed therein a plurality of channels, the apparatus further comprising a plurality of electrically conductive elements, each associated with a respective one of the channels, wherein the cross-sectional shape and dimensions of the channel and the cross-sectional shape and dimensions of the electrically conductive element substantially correspond.
  • the electrically conductive element comprises a conductive polymer material, the conductive element is formed into the said shape and dimension by forming the said conductive polymer material.
  • the electrically conductive polymer may be formed into shape by extruding or moulding, for example.
  • the electrically conductive element is preferably formed such that it yields when subjected to a load, for example when a helicopter lands on the apparatus and rests upon one or more of the electrically conductive elements those elements yield in reacting to the force exerted thereon by the helicopter.
  • an electrical conductor which advantageously is metallic, is encased in the conductive polymer material, and more preferably the electrical conductor is in the form of a wire or a mesh.
  • the electrical conductor extends longitudinally through the conductive polymer.
  • the electrical conductor may be situated towards the centre of the conductive element, or may be situated towards an outer face of the conductive element. More preferably, the electrical conductor is situated just below the upper surface of the electrically conductive element. Still more preferably, the electrical conductor is situated approximately 0.5mm below a surface, preferably the upper surface, of the conductive element.
  • the electrically conductive polymer may comprise a polymer loaded with carbon black.
  • the conductive polymer may comprise a polymer loaded with small metal pieces, such as metal filaments.
  • the electrically conductive elements are so shaped and dimension that when installed in one of the said channels in the base, the upper surface of the electrically conductive element lies in substantially the same plane as the upper surface of the base and advantageously, protrudes just above the upper surface of the base. This ensures good contact between the bird's foot and the electrically conductive elements.
  • the channels and the electrically conductive elements have a dovetail cross- sectional shape.
  • the electrically conductive elements each comprise upper and lower surfaces extending between spaced apart side walls. Preferably, at least the corners where the lower surface joins the side walls are rounded. This provides the advantage that the electrically conductive elements may be more easily inserted into and removed from the base.
  • the base may be formed of a rubber material, which is preferably strongly resilient and hard.
  • the base includes drain holes.
  • the base is advantageously formed of a material which is sufficiently deformable to allow the base to adopt a shape substantially corresponding to the shape of the surface upon which it is laid.
  • the apparatus is laid out on a surface an attached thereto by means of adhesive.
  • adjacent electrically conductive elements are connected alternately to a positive electrical current and to earth, or a negative electrical current respectively.
  • electric current passes from the positively charged element, through the bird, to the earthed or negatively charged element.
  • the electric current discharging through the bird is sufficient to shock, but not kill the bird.
  • the apparatus By mounting the electrically conductive elements in channels formed in a base, and by forming the electrically conductive elements in a shape corresponding to the shape of the channels, the apparatus is capable supporting very heavy loads. For example, the apparatus may be laid out on a helicopter landing pad, and a helicopter may land upon it, without causing significant damage.
  • a switch would be provided in the electrical supply to the apparatus.
  • the electrical supply may then be switched off when personnel need to walk over the apparatus to and from the helicopter.
  • the apparatus may be deployed around the edges of buildings, or on ledges in the same way that other devices of the prior art are deployed.
  • the apparatus may comprise two or three or four channels for example, with the size of the base being specified to fit on the surface where the apparatus is to be used.
  • the materials from which the base and the electrically conductive element are formed need not be so strong, since they would not need to carry the weight of a large vehicle.
  • the material of the base may be specified such that it allows the apparatus to rolled up.
  • Figure 1 is an end view of the mat in its assembled form
  • Figure 2 is an end exploded view of the mat illustrated in Figure 1;
  • Figure 3 is a cross-sectional elevation of an electrically conductive element of the mat illustrated in Figures 1 or 2;
  • Figure 4 is schematic representation of the mat illustrated in Figures 1 to 3;
  • Figure 5a is a schematic representation of an alternative embodiment of the invention.
  • Figure 5b is a schematic representation resembling more closely the actual size of the mat and its component parts.
  • a mat 1 comprising a base 2 formed of a non-conductive material, such as rubber or neoprene for example and having formed therein a series of channels 3.
  • a base 2 formed of a non-conductive material, such as rubber or neoprene for example and having formed therein a series of channels 3.
  • the shape of the channels is dove-tailed in cross-section.
  • the channels 3 receive electrically conductive elements 4, which in the present example comprise a metallic conductive wire 5, formed of copper for example, surrounded by a conductive polymer 6.
  • the conductive polymer 6 allows the conductive element 4 to be formed into a dove -tailed shape that is dimensioned so as to fit tightly into a channel 3.
  • the mat 1 is preferably assembled by aligning the conductive elements 4 with the channels 3 of the base 2, such that the elements 4 are positioned above the channels 3.
  • the base 2 and elements 4 are then passed between rollers resulting in the elements 4 being pressed into the channels 3.
  • the shape of the channels 3 and the corresponding shape of the conductive elements 4 provides two advantages. First, the conductive elements are conveniently secured in the base 2 without the need for any adhesives or other fasteners, and second the manner of securing the conductive element 4 in the base 2 means that the greater the amount of force exerted on the upper surface of the mat 1, the more securely the conductive elements 4 are held in place, whether the force exerted on the mat is exerted between or on the conductive elements 2.
  • edges 7 of the conductive elements 3 are rounded, which facilitates insertion and removal of the conductive elements from the base.
  • the distance between the conductive elements 4 is small, thereby minimising the possibility of a bird landing on the mat and failing to extend a foot across two adjacent conductive elements 4.
  • the upper surface of the conductive element may be approximately 7 mm, and distance between adjacent conductive elements may be approximately 13 mm.
  • the mat 1 is laid on a surface, for example, the upper surface of a helicopter landing pad, such as might be found on an oil rig, or the flight deck of an aircraft carrier.
  • the base 2 may be provided with drainage holes 8, which in use are aligned with drainage channels of a supporting structure.
  • the mat 1 may be attached to a surface by means of adhesive.
  • the surface to which the mat is to be attached is cleaned, adhesive is applied to the underside of the mat (without applying adhesive over the drainage holes 6) and/or the surface to which the mat is to be attached.
  • the mat is then presented to the said surface, pressed down firmly to remove any air bubbles and the adhesive is allowed to cure.
  • Figures 5a and 5b illustrate an alternative embodiment of a mat of the invention. Parts common to the embodiment illustrated in Figures 5a and 5b and the embodiment illustrated in Figures 1 to 4 have been given like reference numerals, with the addition of the symbol ' to the reference numerals in Figures 5a and 5b.
  • the electrically conductive elements 4 comprise a metallic conductive wire 5 surrounded by a conductive polymer 6, in the embodiment of Figures 5a and 5b the conductive element 4' comprises a metallic mesh 5' surrounded by conductive polymer 6'.
  • the conductive polymer 6' may be of the same formulation as described above.
  • the metallic mesh 5' is substantially flat and is situated just below the upper surface of the conductive polymer 6', in fact the metallic mesh 5' is situated about 0.5mm below the surface of the conductive polymer 6'.
  • the conductive polymer 6' allows the conductive element 4' to be formed into a dove-tailed shape that is dimensioned so as to fit tightly into a channel 3'.
  • Figure 5b shows the mat 1' in a scale closer to actual size than the scale indicated in Figure 5a. In actual size, the conductive elements 4' and the base 2' are not as deep as indicated in Figure 5a.
  • the mat of the invention is sufficiently strong to bear the weight of an aircraft, such as a helicopter, without damage occurring to the copper wire encased in the conductive polymer.

Landscapes

  • Life Sciences & Earth Sciences (AREA)
  • Birds (AREA)
  • Engineering & Computer Science (AREA)
  • Insects & Arthropods (AREA)
  • Pest Control & Pesticides (AREA)
  • Wood Science & Technology (AREA)
  • Zoology (AREA)
  • Environmental Sciences (AREA)
  • Catching Or Destruction (AREA)

Abstract

An electric shock delivery apparatus comprises a base (2) of an electrically insulating material, the base having formed therein a plurality of channels (3). The apparatus further comprises a plurality of electrically conductive elements (4), each associated with a respective one of the channels. The cross-sectional shape and dimensions of the channel and the cross-sectional shape and dimensions of the electrically conductive element substantially correspond.

Description

Improved Apparatus for Delivering an Electric Shock Field of the Invention
The present invention relates to an apparatus for repelling birds, and in particular to an apparatus for repelling birds capable of supporting significant weight.
Background of the Invention
Birds often perch on upward facing surfaces of buildings, and can in the process cause a nuisance. Whilst significant problems may be caused to buildings, the problem of nuisance birds is even greater where the surface landed upon by the birds is one used by aircraft for the purpose of landing and take-off. In this situation, the presence of birds may be extremely dangerous.
Helicopter landing pads present a particular problem, especially those located on oil rigs, since the oil rig is likely to be the only structure within a large area upon which sea birds may land. Furthermore, they present a very harsh environment in which to operate any apparatus.
Other forms of vermin also present problems which may be addressed by the use of apparatus for delivering an electric shock to the vermin in question. For example, such apparatus may be used to deter rats from entering buildings.
A number of solutions to the above-mentioned problem have been posed. For example, United States Patent 6,006,698 describes an electrical bird repelling device comprising a base made of an insulating material, and one or more electrically conductive rails disposed on the base. An electric potential is applied to each of the rails such that there is a potential difference between the two rails. When a bird lands on the electrical device and bridges the two rails, current flows between the two rails and the bird is given a mild electric shock which repels the bird from the area of the electrical device. In the device described in US 6,006,698 the electrically conducting metal rails equipped with blades are laid in a base material formed of a polyvinyl chloride (PVC) extruded profile having a hardness of 83. The base has a very low height (2.4mm) the purpose of which is to assist the device blending in with the surface from which birds are to be deterred. The upstanding spikes prevent nesting on the device and are also said to create a noise that is disliked by birds.
DE29610206U1 describes another electric-shock device adapted to deter birds, and comprises a base upon which are mounted alternate positive and negative upstanding tracks. This device is adapted to be mounted on edges of buildings and the like to prevent birds perching thereon.
Keeping surfaces that are to be landed on by aircraft free of birds presents particular problems. Using an electric shock deterrent, one must either rely on a device of the type described above in US 6,006,698 laid on the edge of the surface to deter birds from landing on the whole surface, or alternatively, the device must be either be embedded into the surface, or the device must at least partially cover the surface.
EPl 382243 describes an electric-shock sheet which may be laid out across a surface to be kept free of birds, or other vermin. However, such a sheet is not capable of supporting a significant weight without itself being damaged.
DE G 9405347 describes an electrified mat to protect against animals and adapted to be laid out across a surface, such as the floor of a garage or carport. The mat is laid out across the surface and a car may drive over it. The mat comprises a carrier layer 2 and electrified zones 3, which are isolated from each other. The car driver switches off the electrical supply to the mat to reach the vehicle parked in the garage. The construction of the electrified mat in DE G 9405347 comprises a base, a plurality of exposed live wires extending one way across the carrier layer and a plurality of spaced apart clips extending normal to the direction of the live wires and holding them in place. Whilst the mat described in DE G 9405347 does relate to a mat for use on surface, and for a vehicle to traverse over the mat, the mat is intended for use indoors. The arrangement of the wires would not be conducive to a long service life outdoors. Further, the mat would not appear from the drawings to have significant strength.
It would therefore be desirable to provide an improved apparatus for delivering an electric shock.
Summary of the Invention
According to the invention there is provided an electric shock delivery apparatus comprising a base of an electrically insulating material, the base having formed therein a plurality of channels, the apparatus further comprising a plurality of electrically conductive elements, each associated with a respective one of the channels, wherein the cross-sectional shape and dimensions of the channel and the cross-sectional shape and dimensions of the electrically conductive element substantially correspond.
Advantageously, the electrically conductive element comprises a conductive polymer material, the conductive element is formed into the said shape and dimension by forming the said conductive polymer material. The electrically conductive polymer may be formed into shape by extruding or moulding, for example.
The electrically conductive element is preferably formed such that it yields when subjected to a load, for example when a helicopter lands on the apparatus and rests upon one or more of the electrically conductive elements those elements yield in reacting to the force exerted thereon by the helicopter.
Preferably, an electrical conductor, which advantageously is metallic, is encased in the conductive polymer material, and more preferably the electrical conductor is in the form of a wire or a mesh. Preferably, the electrical conductor extends longitudinally through the conductive polymer. The electrical conductor may be situated towards the centre of the conductive element, or may be situated towards an outer face of the conductive element. More preferably, the electrical conductor is situated just below the upper surface of the electrically conductive element. Still more preferably, the electrical conductor is situated approximately 0.5mm below a surface, preferably the upper surface, of the conductive element.
The electrically conductive polymer may comprise a polymer loaded with carbon black. Alternatively, the conductive polymer may comprise a polymer loaded with small metal pieces, such as metal filaments.
Preferably, the electrically conductive elements are so shaped and dimension that when installed in one of the said channels in the base, the upper surface of the electrically conductive element lies in substantially the same plane as the upper surface of the base and advantageously, protrudes just above the upper surface of the base. This ensures good contact between the bird's foot and the electrically conductive elements.
Advantageously, the channels and the electrically conductive elements have a dovetail cross- sectional shape.
The electrically conductive elements each comprise upper and lower surfaces extending between spaced apart side walls. Preferably, at least the corners where the lower surface joins the side walls are rounded. This provides the advantage that the electrically conductive elements may be more easily inserted into and removed from the base.
The base may be formed of a rubber material, which is preferably strongly resilient and hard. In one embodiment the base includes drain holes. The base is advantageously formed of a material which is sufficiently deformable to allow the base to adopt a shape substantially corresponding to the shape of the surface upon which it is laid.
Preferably, in use the apparatus is laid out on a surface an attached thereto by means of adhesive.
In use, adjacent electrically conductive elements are connected alternately to a positive electrical current and to earth, or a negative electrical current respectively. In this way, when a bird lands on the apparatus with its feet straddling adjacent electrically conductive elements electric current passes from the positively charged element, through the bird, to the earthed or negatively charged element. Preferably, the electric current discharging through the bird is sufficient to shock, but not kill the bird.
By mounting the electrically conductive elements in channels formed in a base, and by forming the electrically conductive elements in a shape corresponding to the shape of the channels, the apparatus is capable supporting very heavy loads. For example, the apparatus may be laid out on a helicopter landing pad, and a helicopter may land upon it, without causing significant damage.
Where the apparatus is deployed on a surface over which personnel are required to walk, for example a helicopter landing pad, a switch would be provided in the electrical supply to the apparatus. The electrical supply may then be switched off when personnel need to walk over the apparatus to and from the helicopter.
Use of the ramp is not confined to use on helicopter landing pads or take-off and landing facilities for other types of aircraft. The apparatus may be deployed around the edges of buildings, or on ledges in the same way that other devices of the prior art are deployed. In such an example, the apparatus may comprise two or three or four channels for example, with the size of the base being specified to fit on the surface where the apparatus is to be used. For such uses the materials from which the base and the electrically conductive element are formed need not be so strong, since they would not need to carry the weight of a large vehicle. Further, the material of the base may be specified such that it allows the apparatus to rolled up.
Brief Description of the Drawings
In the drawings, which illustrate preferred embodiments of an apparatus for delivering an electric shock according to the invention, and are by way of example:
Figure 1 is an end view of the mat in its assembled form;
Figure 2 is an end exploded view of the mat illustrated in Figure 1;
Figure 3 is a cross-sectional elevation of an electrically conductive element of the mat illustrated in Figures 1 or 2;
Figure 4 is schematic representation of the mat illustrated in Figures 1 to 3;
Figure 5a is a schematic representation of an alternative embodiment of the invention;
Figure 5b is a schematic representation resembling more closely the actual size of the mat and its component parts.
Detailed Description of the Preferred Embodiments
Referring now to Figures 1 and 2, the apparatus according to the invention is embodied in a mat 1 comprising a base 2 formed of a non-conductive material, such as rubber or neoprene for example and having formed therein a series of channels 3. As can be seen from Figures 1 and 2, the shape of the channels is dove-tailed in cross-section. The channels 3 receive electrically conductive elements 4, which in the present example comprise a metallic conductive wire 5, formed of copper for example, surrounded by a conductive polymer 6. The conductive polymer 6 allows the conductive element 4 to be formed into a dove -tailed shape that is dimensioned so as to fit tightly into a channel 3.
The mat 1 is preferably assembled by aligning the conductive elements 4 with the channels 3 of the base 2, such that the elements 4 are positioned above the channels 3. The base 2 and elements 4 are then passed between rollers resulting in the elements 4 being pressed into the channels 3.
The shape of the channels 3 and the corresponding shape of the conductive elements 4 provides two advantages. First, the conductive elements are conveniently secured in the base 2 without the need for any adhesives or other fasteners, and second the manner of securing the conductive element 4 in the base 2 means that the greater the amount of force exerted on the upper surface of the mat 1, the more securely the conductive elements 4 are held in place, whether the force exerted on the mat is exerted between or on the conductive elements 2.
As can be seen from Figure 3, the edges 7 of the conductive elements 3 are rounded, which facilitates insertion and removal of the conductive elements from the base.
The distance between the conductive elements 4 is small, thereby minimising the possibility of a bird landing on the mat and failing to extend a foot across two adjacent conductive elements 4. For example, the upper surface of the conductive element may be approximately 7 mm, and distance between adjacent conductive elements may be approximately 13 mm.
The mat 1 is laid on a surface, for example, the upper surface of a helicopter landing pad, such as might be found on an oil rig, or the flight deck of an aircraft carrier. As can be seen from Figure 4, the base 2 may be provided with drainage holes 8, which in use are aligned with drainage channels of a supporting structure.
The mat 1 may be attached to a surface by means of adhesive. The surface to which the mat is to be attached is cleaned, adhesive is applied to the underside of the mat (without applying adhesive over the drainage holes 6) and/or the surface to which the mat is to be attached. The mat is then presented to the said surface, pressed down firmly to remove any air bubbles and the adhesive is allowed to cure.
Figures 5a and 5b illustrate an alternative embodiment of a mat of the invention. Parts common to the embodiment illustrated in Figures 5a and 5b and the embodiment illustrated in Figures 1 to 4 have been given like reference numerals, with the addition of the symbol ' to the reference numerals in Figures 5a and 5b.
The principal difference between the embodiment of Figures 1 to 4 and the embodiments of Figures 5a and 5b lies in the construction of the conductive elements. Whereas in Figures 1 to 4 the electrically conductive elements 4 comprise a metallic conductive wire 5 surrounded by a conductive polymer 6, in the embodiment of Figures 5a and 5b the conductive element 4' comprises a metallic mesh 5' surrounded by conductive polymer 6'. The conductive polymer 6' may be of the same formulation as described above. In the example, the metallic mesh 5' is substantially flat and is situated just below the upper surface of the conductive polymer 6', in fact the metallic mesh 5' is situated about 0.5mm below the surface of the conductive polymer 6'.
As with the embodiment illustrated in Figures 1 to 4, the conductive polymer 6' allows the conductive element 4' to be formed into a dove-tailed shape that is dimensioned so as to fit tightly into a channel 3'. Figure 5b shows the mat 1' in a scale closer to actual size than the scale indicated in Figure 5a. In actual size, the conductive elements 4' and the base 2' are not as deep as indicated in Figure 5a.
The mat of the invention is sufficiently strong to bear the weight of an aircraft, such as a helicopter, without damage occurring to the copper wire encased in the conductive polymer.

Claims

Claims
1. An electric shock delivery apparatus comprising a base of an electrically insulating
material, the base having formed therein a plurality of channels, the apparatus further comprising a plurality of electrically conductive elements, each associated with a respective one of the channels, wherein the cross-sectional shape and dimensions of the channel and the cross-sectional shape and dimensions of the electrically conductive element substantially correspond.
2. Apparatus according to Claim 1, wherein the electrically conductive element comprises a conductive polymer material, the conductive element is formed into the said shape and dimension by forming the said conductive polymer material.
3. Apparatus according to Claim 1 or 2, wherein the material properties of the conductive element are such that the said conductive element yields when subjected to a load.
4. Apparatus according to any preceding claim, wherein the electrically conductive element further comprises an electrical conductor encased in the conductive polymer material.
5. Apparatus according to Claim 4, wherein the electrical conductor is a wire or a mesh.
6. Apparatus according to Claim 4 or 5, wherein the electrical conductor is metallic.
7. Apparatus according to any of Claims 4 to 6, wherein the electrical conductor is situated towards the upper surface of the electrically conductive element.
8. Apparatus according to any of Claims 4 to 6, wherein the electrical conductor is situated substantially centrally in the electrically conductive element.
9. Apparatus according to any of Claims 2 to 8, wherein the electrically conductive polymer comprises a polymer loaded with carbon black and/or small metal pieces.
10. Apparatus according to any preceding claims, wherein the electrically conductive
elements are so shaped and dimension that when installed in one of the said channels in the base, the upper surface of the electrically conductive element lies in substantially the same plane as the upper surface of the base.
11. Apparatus according to Claim 10, wherein the upper surface of the electrically conductive element protrudes just above the upper surface of the base.
12. Apparatus according to any preceding claims, wherein the channels and the electrically conductive elements have a dovetail cross-sectional shape.
13. Apparatus according to any preceding claim, wherein the electrically conductive
elements each comprise upper and lower surfaces extending between spaced apart side walls, wherein at least the corners where the lower surface joins the side walls are rounded.
14. Apparatus according to any preceding claim, wherein the base is formed of a rubber material.
15. Apparatus according to any preceding claim, wherein the material from which the base is formed is strongly resilient.
16. Apparatus according to any preceding claim, further comprising electrical connections to each of the electrically conductive elements, wherein adjacent electrically conductive elements are connected alternately to a positive electrical current and to earth, or a negative electrical current respectively.
17. Apparatus substantially as shown in, and as described with reference to, the drawings.
PCT/GB2010/051284 2009-08-04 2010-08-04 Improved apparatus for delivering an electric shock WO2011015867A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US13/388,543 US20120127624A1 (en) 2009-08-04 2010-08-04 Apparatus for delivering an electric shock
EP10742538.1A EP2461674B1 (en) 2009-08-04 2010-08-04 Improved apparatus for delivering an electric shock

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0913534.4 2009-08-04
GBGB0913534.4A GB0913534D0 (en) 2009-08-04 2009-08-04 Improved apparatus for delivering an electric shock

Publications (1)

Publication Number Publication Date
WO2011015867A1 true WO2011015867A1 (en) 2011-02-10

Family

ID=41129567

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB2010/051284 WO2011015867A1 (en) 2009-08-04 2010-08-04 Improved apparatus for delivering an electric shock

Country Status (4)

Country Link
US (1) US20120127624A1 (en)
EP (1) EP2461674B1 (en)
GB (1) GB0913534D0 (en)
WO (1) WO2011015867A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2492549A (en) * 2011-07-04 2013-01-09 P & L Systems Ltd Deterrent Device
US8640380B2 (en) 2011-10-19 2014-02-04 P & L Systems Limited Deterrent device

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013052073A1 (en) 2011-10-04 2013-04-11 Bird-B-Gone, Inc. Electrified bird deterrent device with treads
US9585377B1 (en) * 2016-06-16 2017-03-07 Ratio Engineering LLC Fencing apparatus and system
US10420334B2 (en) 2016-07-19 2019-09-24 Steven V. Oliveira Rodent barrier system and method
JP6464328B1 (en) * 2017-06-05 2019-02-06 將二 寺田 Self-defense threat repelling device

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990011001A1 (en) * 1989-03-13 1990-09-20 Raychem Corporation Method of making an electrical device comprising a conductive polymer
DE9405347U1 (en) 1994-03-30 1994-05-26 Horizont Gerätewerk GmbH, 34497 Korbach Electric mat
DE29610206U1 (en) 1996-06-11 1996-10-24 AHRENS Bautechnologie Handelsgesellschaft mbH, 61118 Bad Vilbel Electrical protection against birds
US6006698A (en) 1996-12-11 1999-12-28 Societe Ecopic Line S.A.R.L. Electrical device for repelling birds
EP1382243A1 (en) 2001-04-23 2004-01-21 Junzo Toyota Rat exterminating electroshock sheet, and method of expelling harmful birds and animals
WO2005055865A2 (en) * 2003-12-04 2005-06-23 Bird Barrier America, Inc. Electric deterrent device
US20050183880A1 (en) * 2004-02-19 2005-08-25 Waldorf Philip M. Anti-roosting device
US20100180490A1 (en) * 2009-01-19 2010-07-22 Bird-B-Gone, Inc. Electric Deterrent Device Having Knitted Conductors

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2184392A (en) * 1937-01-07 1939-12-26 Anaconda Wire & Cable Co Hollow conductor
ATE86040T1 (en) * 1985-06-12 1993-03-15 Raychem Corp HYDROCARBON SENSOR.
DE3930013A1 (en) * 1989-09-08 1991-03-14 Windhager Trading & Consulting Snail defence band - with ribs carrying a pair of live semiconductor cables
DE20016374U1 (en) * 2000-09-21 2000-12-14 Schuster, Harald, 63128 Dietzenbach Bird control device
CN101101799A (en) * 2006-07-07 2008-01-09 鸿富锦精密工业(深圳)有限公司 Electric wire and its combination

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990011001A1 (en) * 1989-03-13 1990-09-20 Raychem Corporation Method of making an electrical device comprising a conductive polymer
DE9405347U1 (en) 1994-03-30 1994-05-26 Horizont Gerätewerk GmbH, 34497 Korbach Electric mat
DE29610206U1 (en) 1996-06-11 1996-10-24 AHRENS Bautechnologie Handelsgesellschaft mbH, 61118 Bad Vilbel Electrical protection against birds
US6006698A (en) 1996-12-11 1999-12-28 Societe Ecopic Line S.A.R.L. Electrical device for repelling birds
EP1382243A1 (en) 2001-04-23 2004-01-21 Junzo Toyota Rat exterminating electroshock sheet, and method of expelling harmful birds and animals
WO2005055865A2 (en) * 2003-12-04 2005-06-23 Bird Barrier America, Inc. Electric deterrent device
US20050183880A1 (en) * 2004-02-19 2005-08-25 Waldorf Philip M. Anti-roosting device
US20100180490A1 (en) * 2009-01-19 2010-07-22 Bird-B-Gone, Inc. Electric Deterrent Device Having Knitted Conductors

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2492549A (en) * 2011-07-04 2013-01-09 P & L Systems Ltd Deterrent Device
WO2013005006A1 (en) * 2011-07-04 2013-01-10 P & L Systems Limited Deterrent device
GB2492549B (en) * 2011-07-04 2015-08-26 Pelsis Ltd Deterrent Device
US8640380B2 (en) 2011-10-19 2014-02-04 P & L Systems Limited Deterrent device

Also Published As

Publication number Publication date
US20120127624A1 (en) 2012-05-24
EP2461674B1 (en) 2015-07-15
GB0913534D0 (en) 2009-09-16
EP2461674A1 (en) 2012-06-13

Similar Documents

Publication Publication Date Title
EP2461674B1 (en) Improved apparatus for delivering an electric shock
US7249436B2 (en) Electric shock bird and animal deterrent
US10106935B1 (en) Electrically-grounded work platform
US20050132636A1 (en) Flexible apparatus cover providing electrical shock upon contact
US9277742B2 (en) Electrified bird deterrent device with treads
US7299586B2 (en) Antipest mat
CA2809517C (en) Elevated platform systems including fiber reinforced composite panels
US20210368777A1 (en) Shockem Rodent Deterrent System
US20070131666A1 (en) Heated mat apparatus
DE102006051662B4 (en) Apparatus for deterring small mammals
WO2007010282A1 (en) Electrical apparatus for repelling birds
US20230117979A1 (en) Electrically Conductive Surface And A Process For Producing The Same
GB2518368A (en) Pest deterrent barriers
DE202006003419U1 (en) Device for giving electric shocks to small mammals comprises a current source connected to electrodes on an electrode carrier, or to electrodes appropriately distanced from one another
AU2018100762A4 (en) Electrical barrier
KR102589342B1 (en) Electric shock type birds repeller
DE10139281A1 (en) Bird repelling device, has plastics material of profile- sections partly enclosing spaced electrical wires
DE102010019921A1 (en) Mass mat for small animal quenching
JP2005216503A (en) Shielding plate for preventing feces harm
KR20100009115U (en) Apparatus for preventing a nest building
ZA200909142B (en) Animal deterring device

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 10742538

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 13388543

Country of ref document: US

NENP Non-entry into the national phase

Ref country code: DE

WWE Wipo information: entry into national phase

Ref document number: 2010742538

Country of ref document: EP