EP1158263A1 - Conteneur pour un fluide susceptible d'être dispersé dans l'air libre et dispositif de défense comportant un tel conteneur - Google Patents

Conteneur pour un fluide susceptible d'être dispersé dans l'air libre et dispositif de défense comportant un tel conteneur Download PDF

Info

Publication number
EP1158263A1
EP1158263A1 EP00810459A EP00810459A EP1158263A1 EP 1158263 A1 EP1158263 A1 EP 1158263A1 EP 00810459 A EP00810459 A EP 00810459A EP 00810459 A EP00810459 A EP 00810459A EP 1158263 A1 EP1158263 A1 EP 1158263A1
Authority
EP
European Patent Office
Prior art keywords
nozzle
unit
piston
self
storage
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Withdrawn
Application number
EP00810459A
Other languages
German (de)
English (en)
Inventor
Raphael Fleischhauer
Jürg Thomann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Piexon AG
Original Assignee
Piexon AG
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 Piexon AG filed Critical Piexon AG
Priority to EP00810459A priority Critical patent/EP1158263A1/fr
Priority to PCT/CH2001/000319 priority patent/WO2001090674A1/fr
Priority to AT01929163T priority patent/ATE321989T1/de
Priority to RU2002135081/02A priority patent/RU2269082C2/ru
Priority to CZ20023564A priority patent/CZ20023564A3/cs
Priority to CNB018132669A priority patent/CN1205456C/zh
Priority to BRPI0111178-7A priority patent/BR0111178B1/pt
Priority to DE50109382T priority patent/DE50109382D1/de
Priority to US10/296,399 priority patent/US6951070B2/en
Priority to KR1020027015967A priority patent/KR20030005400A/ko
Priority to EP01929163A priority patent/EP1285217B1/fr
Priority to AU2001256047A priority patent/AU2001256047A1/en
Priority to IL15304201A priority patent/IL153042A0/xx
Publication of EP1158263A1 publication Critical patent/EP1158263A1/fr
Priority to ZA200209603A priority patent/ZA200209603B/en
Priority to US11/208,514 priority patent/US7316090B2/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41BWEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE; WEAPONS NOT OTHERWISE PROVIDED FOR
    • F41B9/00Liquid ejecting guns, e.g. water pistols, devices ejecting electrically charged liquid jets, devices ejecting liquid jets by explosive pressure
    • F41B9/0003Liquid ejecting guns, e.g. water pistols, devices ejecting electrically charged liquid jets, devices ejecting liquid jets by explosive pressure characterised by the pressurisation of the liquid
    • F41B9/0031Liquid ejecting guns, e.g. water pistols, devices ejecting electrically charged liquid jets, devices ejecting liquid jets by explosive pressure characterised by the pressurisation of the liquid the liquid being pressurised at the moment of ejection
    • F41B9/0043Pressurisation by explosive pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H9/00Equipment for attack or defence by spreading flame, gas or smoke or leurres; Chemical warfare equipment
    • F41H9/10Hand-held or body-worn self-defence devices using repellant gases or chemicals

Definitions

  • the invention relates to a storage unit for an expellable in the free space Active ingredient according to the preamble of claim 1 and a self-defense device with this storage unit according to the preamble of the claim 6.
  • a non-generic storage unit as a disposable syringe, from which an active ingredient by means of a propellant to be ignited from a storage space through a channel injected under the human skin is, for example, from the US-A 4 124 024, US-A 4 089 334, US-A 3802 430 and US-A 3 335 722 known.
  • US-A 4 089 334 describes a disposable syringe in which a vaccine without Needle is "shot" directly through the skin.
  • the vaccine was in one with a piston locked cylinder.
  • the cylinder side opposite the piston had at least one opening through which the vaccine, after igniting one Propellant could leak. The ignition took place with a blow fuse.
  • a disposable syringe without an injection needle is known from US Pat. No. 4,124,024. in which the active ingredient is injectable through the skin into human tissue was.
  • the disposable syringe had a protective capsule on the outside tapered outlet channel.
  • the exit channel was at its base with a rupture disc.
  • the storage space for the active ingredient went from an im Cross-section of a circular cylindrical part in a conically tapering, at its narrowest Place the rupture sheath over.
  • the active ingredient to be injected was between a piston and this rupture disc included.
  • the piston surface had a frustoconical shape adapted to the tapering of the storage space Training, arranged on the upper truncated cone surface a cone pyramid was.
  • the other piston surface was concave. Between the concave Piston area and the igniter of an impact igniter was a space for pressure build-up the propellant gases present after ignition against the piston.
  • the object of the invention is a safe, simple use of a storage unit to ensure that the active ingredient stored in it is not in a sealing Contact between the outlet channel and skin is brought under the skin should be, but in a given distribution configuration in the free Room.
  • This storage unit is in a manner not obvious in an inventive Self-defense device can be integrated, even by an untrained Operator is easy to operate and also not as a "hand gun" from is recognizable to a potential opponent.
  • the Propellant charge are oversized. I.e. the propellant charge cannot be selected in this way that it would only be sufficient to drive off the active ingredient. It a certain overpressure must therefore be present. This overpressure is then through a special embodiment described below of the active ingredient expelling Piston and the accumulator wall dismantled in that this through the nozzle channels can discharge.
  • the closure element already mentioned above closes all nozzle channels.
  • the closure element designed as a rupture disc is torn open in such a way that the Fractions remain well secured around their edges. The tearing also takes place such that the fragments do not hinder the flow of active ingredient to the nozzles.
  • the rupture disc can also have notched areas or areas with thinned material have a predetermined opening.
  • the storage unit is used, for example, in a self-defense device used, as uniform as possible over a predetermined period of time Expulsion of the active ingredient may be given.
  • This steady expulsion will one day in that a nozzle antechamber is achieved between the rupture disc and the nozzle inlets is provided, which among other things acts as a calming room.
  • the active ingredient only flows into this space, causing Pressure peaks of the active ingredient and turbulence are largely eliminated become.
  • the "calmed" active ingredient only then hits the nozzles and can do so then leave in the desired configuration.
  • the storage unit If the storage unit is integrated into a self-defense device, it should also the configuration of the emerging active ingredient, mainly that of the attacker directed jet have a constant pressure as possible. To the even To continue to drive out, the propellant charge is oversized. In addition is an expansion space between the piston surface expelling the active ingredient and the Propellant charge present. As a result, the first pressure peak is intercepted the ignition, which is an expulsion with an approximately constant force and thus with a constant active ingredient configuration in free space over the expulsion period.
  • a nozzle unit with at least one main nozzle and at least one in which As a rule, however, design with several secondary nozzles arranged around them.
  • the storage unit is used in a self-defense device, then an irritant liquid or an irritant gas is used as the active ingredient; but it can also powdery substances are used.
  • the storage unit 1 shown in cross section in FIGS. 1 and 2 is designed as a so-called cartridge and is preferably used in a self-defense device.
  • the cartridge 1 has a nozzle unit 3 on the left in FIGS. 1 and 2 .
  • the cartridge 1 has a storage space 5 , a propellant charge 7 and an ignition charge 9 for igniting the propellant charge 7 .
  • FIGS. 1 and 2 also show a mechanical percussion ignition unit 10 , which, however, is part of the self-defense device 11 described below.
  • the whipping unit 13 of the Schlagzündtechnik 10 is held in its rest state shown in Figure 1 in a snap to grid 14th
  • the impact unit 13 can be rotated with a mechanism described below from the catch 14 for release into a free impact path.
  • powdery, gaseous and / or liquid active substances 15 can be stored in the storage space. Mixtures between powdery, gaseous and / or liquid different active ingredient components can also be incorporated.
  • a liquid active substance 15 is stored. Since the storage unit 1 is to be integrated into a self-defense device 11 as described below, the active ingredient 15 is to have an immediate effect on the mucous membranes (eyes, respiratory tract) of a potential attacker.
  • the storage space 5 filled with the active substance 15 is closed towards the nozzle unit 3 with a closure element 19 having material dilution lines 17 . In the non-ignited state, the closure element 19 prevents the active substance 15 from escaping from the storage space 5 through the nozzle unit 3 .
  • the storage space 5 is sealed gas-tight against the propellant charge 7 with a piston 21 fixed in the clamped fit in the cylindrical wall 20 of the storage space 5 .
  • the piston 21 is cup-shaped with a cup bottom 22 and a cup jacket 23 .
  • the piston 21 is also referred to as a sabot.
  • the cup interior 24 as a free space between the propellant charge 7 and the cup base 22 connected to the active substance 15 serves as an expansion space 24 in order to obtain the most uniform possible forward movement of the piston 21 after the propellant gases have formed from the ignited propellant charge 7, with the elimination of pressure peaks .
  • the expansion space 24 has a volume which is approximately one eighth of the liquid volume of the active substance 15 .
  • Pressure relief means 27 are arranged in the storage area end region 25 adjacent to the nozzle unit 3.
  • the pressure relief means 27 are designed here, for example, as webs projecting into the storage space end region 25 .
  • the pressure relief means 27 serve to relieve the propellant gas in the storage space 5 after the active ingredient has been completely expelled. The mode of operation is explained below. With the complete breakdown of the residual gases, the last residues of the active ingredient are also blown out of the storage space 5 , the nozzle unit 3 and the nozzle antechamber 29 . The amount of active ingredient can thus be optimally specified.
  • a nozzle antechamber 29 which can act as, among other things, a calming space.
  • the nozzle antechamber 29 is used on the one hand to give space to the parts of the rupture disk 19 that are torn open due to the build-up of pressure without clogging the main and secondary channels 31 and 32 , and on the other hand to calm the accelerated active substance 15 and minimize fluid turbulence.
  • the depth of the nozzle chamber 29 is preferably chosen to be a tolerance deeper than its radius, and is somewhat smaller than the radius of the rupture disk 19 .
  • the rupture disk 19 is thus freely spanned in front of the nozzle antechamber 29 ; their edges, however, are clamped.
  • the rupture disk 19 tears in a star shape after reaching a predetermined gas pressure due to the burning propellant, ie starting nicely from the center.
  • This radial segmental tearing ensures that no fragments of the rupture disk 19 are thrown out of the nozzle unit 3 as solid bodies, since the edges of the rupture disk 19 are still held firmly.
  • the ruptured rupture disc segments then lay against the wall of the nozzle anteroom without clogging the nozzle channels.
  • the nozzle unit 3 has a centrally arranged main nozzle channel 31 and several, here four, coaxially arranged secondary nozzle channels 32 .
  • main nozzle channel 31 and several, here four, coaxially arranged secondary nozzle channels 32 .
  • main nozzle channels 31 there can also be several main nozzle channels and only one secondary nozzle channel.
  • the number and arrangement of the nozzle channels depends on the intended use and a desired spatial distribution of the active ingredient.
  • the four secondary nozzle channels 32 open into an annular space 28 which runs around the main nozzle channel 31 and which has a circumferential incline 30 at which the secondary jets break and atomize in order to "atomize" the liquid emerging from the secondary nozzle channels 32 .
  • the main nozzle channel 31 is designed in such a way that an approximately straight liquid jet emerges from the active substance 15 squeezed out by the propellant gas up to a distance of four meters, which has large drops after being blown off.
  • the secondary nozzle channels 32 are intended to generate a large scatter circle with finely distributed small drops of active liquid as the active substance cloud.
  • the impact unit 13 is unlocked in a first step in a storage unit 1 integrated in a self-defense device 11 .
  • the unlocking is done by unscrewing the catch 14 from its holding position.
  • the impact unit is pushed to the right in FIG. 1 by tensioning a spring 33 and then released. Due to the force of the tensioned spring 33 , the impact bolt 34 of the impact unit 13 is thrown against the primer 7 , which ignites and acts as an initial igniter on the propellant 7 .
  • the propellant charge 7 begins to burn, the propellant gases arising penetrating into the expansion space 24 and after a short period of time the propellant gas expansion force exceeds the clamping force of the piston 21 with the storage space wall 20 , as a result of which the piston 21 is driven in the direction of the nozzle unit 3 .
  • the pressure in the active ingredient 15 suddenly increases. This pressure increase acts on the rupture disk 19 , which tears open along its material thinning lines 17 .
  • the rupture disk 19 is of stable design at its outer edges and is held well in the wall of the nozzle antechamber 29 . It tears open; moving fragments do not occur. As indicated in FIG. 2 , the rupture disk fragments (segments) lie against the wall of the nozzle antechamber 29 .
  • the nozzle antechamber 29 thus enables the desired radial segment-like tearing of the rupture disk 29 , on the other hand it also serves to dampen turbulence in the active liquid. These eddies would in particular negatively influence the range of the liquid jet emerging through the main nozzle channel 31 .
  • the piston 21 enters the storage area end region 25 , it slides over the pressure relief means 27 designed as webs. This slipping causes the piston 21 to be deformed on the one hand and it is braked on the other hand, thereby avoiding a blow to the nozzle unit 3 .
  • the transition between the nozzle unit 3 and the wall 20 must therefore be made less stable, which results in a simpler construction.
  • the deformation of the piston 21 creates lateral channels 35 between the wall 20 and the cup jacket 23 .
  • the remaining propellant gas can then escape through these channels 35 , as indicated by the arrows 37 in FIG .
  • the residual gases are blown out through the nozzle unit 3 . This also completely blows out the nozzle channels in such a way that no residual amount of the active ingredient remains.
  • the self-defense device can be put down in any place, without residues of the active ingredient having any effect.
  • the remaining storage unit 1 is depressurized and therefore easy to handle and store.
  • the above-described configuration of the rupture disk 19 , the nozzle antechamber 29 and also the pressure relief means 27 ensure that no solid parts, such as parts of the nozzle unit 3 , the piston 21 and the rupture disk 19 , can be thrown out during firing.
  • a self-defense device 11 equipped with this storage unit 1 can thus be sold freely, since there is no risk of injury to a bombarded attacker.
  • This storage unit can be used in the invention described below Self-defense device to be integrated. Such integration will solved the task of creating a self-defense device, which on the one hand is easy to use by inexperienced people and no residual risk after "firing" includes.
  • the self-defense device can also be designed in such a way that that it bears no resemblance to a handgun and is still a good aim allowed.
  • WO 98/38468 shows a gun that is not recognizable as a pistol Self-defense device described.
  • the device is a keychain in appearance modeled. It has two barrels, each of which is charged by means of a release button can be triggered per run. Preloadable ones are used to ignite the shooting charge Firing pin available. A solid is fired as a projectile.
  • Self-defense devices designed analogously to this are from the US-A 1 741 902, DE 3 310 155, and FR 776 954 are known.
  • the FR 776 954 permits the use of a variety of cartridges; i.a. also from tear gas cartridges.
  • the task of creating a self-defense device that is easy to use create is solved in that these two symmetrical to a plane of symmetry arranged storage units and only a single deduction for the successive "Fired" storage units with an automatic switch to one then still has to be fired storage unit.
  • the self-defense device is trained in such a way that it can be used by both right-handed and left-handed users. Further advantages of the self-defense device result from the following Text.
  • the self-defense device 11 shown in FIG. 3 has a first plane of symmetry 41, to which a memory unit 1a or 1b , which is not readily recognizable, is symmetrically integrated as a pair. From a close view of the two storage units 1a and 1b , only the nozzle outputs of the respective nozzle unit 3 of the main nozzle channel 31 and the secondary nozzle channels 32 can be seen in a frontal view ( FIG. 5 ).
  • a single operating slide 43 for triggering a storage unit 1a or 1b is arranged in the plane of symmetry 41 .
  • Neglecting a clip (holding unit) 45 for fastening the self-defense device 11 to the clothing of an operator, this self-defense device 11 is also formed symmetrically to a further plane of symmetry 46 shown in FIG.
  • the two planes of symmetry 41 and 46 mainly apply to the housing and the arrangement of the storage unit with the operating slide 43 .
  • the functional elements for the trigger unit 59 are not symmetrical to these planes of symmetry 41 and 46 together.
  • the self-defense device 11 is large palm. It has an opening 47 in the middle in the front area through which the trigger finger can be inserted.
  • the operating slide 43 projects into this opening 47 .
  • the free cross section of the opening 47 is increased as a result of the release path.
  • the opening cross section 47 between the free edge 44 of the operating slide 43 and the opening edge 50 is so large that there is space for a finger to be inserted.
  • the outlet openings of each nozzle unit 3 are integrated in the housing contour.
  • the housing of the self-defense device 11 is of flat design so that it lies well in the palm of the hand and can be worn concealed. There is also an indentation 51a and 51b on both sides for the hand recess between the thumb and index finger.
  • indentations 51a and 51b are required on both sides.
  • the housing is made in two parts.
  • the two housing parts 53a and 53b are fixed to one another, cannot be opened.
  • the connection point between the two housing parts 53a and 53b is a circumferential groove 55 , which lies in the plane of symmetry 46 .
  • This groove 55 crosses the center of the main nozzle channel 31 .
  • This groove 55 runs in the plane of symmetry 46 .
  • This groove 55 can thus be used not only as a visible but also as a tactile target aid to the potential attacker.
  • the appearance of the self-defense device resembles, for example, a dog leash reel-up unit, wallet, credit card pocket, or other objects, but not a handgun. Since the self-defense device 11 is not recognizable as a weapon by a potential attacker, it will also not increase its aggressiveness. On the contrary, the attacker will feel secure and superior. A triggering of the active substance stored in the storage unit 1a or 1b will therefore completely surprise him, whereby escape or countermeasures of the attacked person will be facilitated.
  • the process for firing a first and then a second storage unit 1a and 1b is described below.
  • additional units can of course also be integrated in a variant of a self-defense device.
  • the two storage units, here designated 1a and 1b are ignited in the embodiment variant described below with a mechanical impact detonator.
  • an electrical / mechanical detonator can also be used, as described, for example, in WO 00/06965.
  • FIG. 6 shows the self-defense device 11 shown in FIGS . 3 to 5 in the position shown in FIG. 3 , but with the housing part 53b removed .
  • Figure 7 shows the same, but only the upper half of Figure 6 in an enlarged view.
  • the guide curves 60a and 60b are shown in dashed lines in the removed housing half 53a .
  • the trigger device 59 thus consists of the above-mentioned operating slide (trigger) 43 with an extension bolt 61 , a rotor 63 , a return spring 65 and the above-mentioned two impact units 13 , each with one of the springs 33 .
  • the extension bolt 61 is cylindrical with six coaxially extending, angularly equally spaced webs 67a to 67f , which are separated from one another by grooves 69a to 69f.
  • the axis of the extension bolt 61 is designated 70 .
  • the axis 70 of the extension bolt 61 is aligned with that of the rotor 63 .
  • the webs 67a to 67f and the grooves 69a to 69f can be seen in the right half of the figures 8 to 13 in plan view.
  • FIGS. 8 to 13 show the relative movement sequence of the rotor 63 to the extension bolt 61 and the movement of the impact unit 13b ( FIG. 7 ).
  • the webs 67a to 67f have at their free ends two roof-like bevels 71a and 71b which are symmetrical to one another.
  • the bevels 71a and 71b continue into a V-shaped, symmetrical cut 72 in the grooves 69a to 69f .
  • the rotor 63 has three coaxial webs 75a to 75c equally spaced angularly and three stub webs 76a to 76c arranged centrally to the webs 75a to 75c .
  • the webs 75a to 75c and the stub webs 76a to 76c each have a pent roof-like slope 77 .
  • the bevels 77 of the rotor 63 and the bevels 71a and 71b of the extension bolt 61 engage in cooperation with the guide curves 60a in a manner analogous to the pressure mechanism of a ballpoint pen with an insertable and retractable face.
  • the catch catch already mentioned above is designated 14b here, since it belongs to the storage unit 1b , is guided in the guide curve 60b .
  • the guide curve 60b is not shown in FIGS . 8 to 13 .
  • the propellant gases of the burning propellant 7 then flow into the cup interior 24 serving as an expansion space. If a sufficient propellant gas pressure is built up, the piston 21 , which acts as a propellant, is propelled. The piston 21 presses on the active ingredient 15 , which in turn acts on the closure element 19 acting as a rupture disk. The closure element 19 tears along its material thinning lines 17 ; however, remains on its edges as shown in Figure 2 .
  • the piston 21 is driven by the propellant gases by expelling the active substance 15 through the main nozzle channel 31 and the secondary nozzle channels 32 against the storage area end region 25 . When the storage space end region 25 is reached, the entire piston 21 is deformed by the webs located on the storage wall as a pressure relief means 27 .
  • the side walls 23 of the piston surface 22 are also partially pressed in, as a result of which channels 35 are formed between the piston side wall regions and the accumulator wall in the accumulator end region 25 .
  • the propellant gas can escape through these channels 35 until the pressure is completely released.
  • the operating slide 43 is released, it is brought back into its forward position by the return hollow spring 65 .
  • the webs 75a to 75c and stub webs 76a to 76c slide along a slope 83 of the guide curves 60a , which causes a small further rotation in the direction 82 .
  • the rotor 63 slides axially back to a further slope 84 of the guide curves 60b ( FIG. 12 ).
  • the pitched roof slopes 77 of the webs 75a to 75c and the stub webs 76a to 76c slide on the slopes 71a of the webs 69a to 69f of the extension bolt 61 into a new rest position ( FIG. 13 ).
  • the projection 81a belonging to the impact unit 13a is now ready for renewed engagement with the rotor 63 , so that the other storage unit 1a can be "fired" when the operating slide 43 is pressed in.
  • the material thinning lines 17 can be dispensed with in the closure element 19 .
  • This element 19 is then produced as a thin aluminum disc, the edges of which are no different from the center.
  • grooves 85 can also be formed in the storage wall in the storage space end region 86 there, as shown in FIG .
  • the grooves 85 must then be a tolerance longer than the height d of the piston 87, which is designed analogously to the piston 21 .
  • the piston 87 strikes a shoulder at the end of the storage space. This means that after firing there is a hard blow, while in the embodiment variant described above there is only a gentle blow with the pressure relief means 27 .
  • a self-defense device 90 which has a piezolelectric ignition instead of a mechanical detonator, is shown in longitudinal section in FIG .
  • the outer contour of this self-defense device 90 is identical to that described above.
  • the two storage units 91a and 91b are also identical except for the ignition and propellant charge 93a and 93b .
  • a triggering device 94 of the self-defense device 90 here has, analogously to the self-defense device 11, an operating slide 95 as a "trigger".
  • the operating slide 95 is held in its rest position by a compression spring 96 .
  • An effect on an arrangement 97 with a piezoelectric high-voltage pulse generator and an integrated electrical switchover arrangement takes place only after an indentation path has been overcome.
  • the arrangement 97 is inserted into an electrical circuit board 99 with electrical connections (not shown) to the ignition and propellant charges 93a and 93b .
  • the electro-mechanical structure of this self-defense device 90 is shown schematically in an exploded view in FIG .
  • the two housing parts 53a and 53b are at the top and bottom.
  • the clip 45 is snapped into the housing part 53b ; but it could also be glued or welded to it.
  • a central injection-molded part 100 has a rear cover, which is welded onto the base housing (injection-molded part) 100 in a liquid-tight manner after assembly of the “interior”. Thanks to the likewise watertight sealing rings 105 (sliding seal), the base housing 100 is closed in a liquid-tight manner, which is necessary due to the electromechanics contained therein.
  • the housing parts 53a and 53b thus only have a "body function", since the base housing 100 already contains all the technical functional parts and is closed in a liquid-tight manner.
  • the housing parts 53a and 53b would therefore only have to be clipped together here.
  • the two storage spaces 101a and 101b of the storage units 91a and 91b and a receiving sleeve 103 for the piezoelectric high-voltage generator 104 are also the two storage spaces 101a and 101b of the storage units 91a and 91b and a receiving sleeve 103 for the piezoelectric high-voltage generator 104 .
  • a sealing ring 105 is to be placed on each rupture disk 19 .
  • the nozzle units 3 are located in recesses 109 and 107 of the housing parts 53a and 53b and press sealingly on one of the sealing rings 105 .
  • the operating slide 95 is also sealed off from the inside of the self-defense device 90 by a sealing ring 110 .
  • the operating slide 95 is guided in a box-like casing, only the half-box 111 formed in the housing part 53a being shown in the illustration in FIG. 16 .
  • the operating slide 95 is secured against falling out in the direction of the opening 47 by a lateral elevation 113 , which is formed in a corresponding groove, formed from the half-boxes and the inserted injection molded part 100 in the assembled state.
  • the two pistons 21 are also each sealed by a sealing ring 115 .
  • the storage units 1a, 1b, 91a and 91b according to the invention are used integrated in a self-defense device in the above-mentioned exemplary embodiments.
  • these storage units 1a, 1b, 91a and 91b can also be used in a fixed position in the immediate vicinity of objects at risk.
  • objects can be, for example, showcases, shop windows or entrance doors in jewelry stores, private villas, etc.
  • the primer of the storage units can e.g. B. coupled with a glass break sensor.
  • a glass break sensor As soon as a burglar breaks a window that is secured in this way, a permanently installed storage unit is ignited. The active ingredient then escaping from the storage unit "mists" the space in which the burglar is at that moment. The perpetrator is hereby prevented from doing so and, depending on the active ingredient used, is marked or immobilized for a temporary period.
  • the glass break sensor responds, an alarm is triggered and / or the police are alerted.
  • FIGS. 3 to 7 and 15 and 16 A further variant of a self-defense device 120 to that shown in FIGS. 3 to 7 and 15 and 16 is shown in cross section in FIG .
  • the contour of the housing corresponds to that shown in FIGS. 3 to 5 .
  • the self-defense device 120 does not have a rotating switching mechanism for the ignition of the storage units, but a switching gate 123 . While the rotating changeover takes place three-dimensionally, the shifting gate works two-dimensionally.
  • An operating slide (trigger) 124 made of plastic has two resilient arms 125a and 125b and is held in its rest position by a compression spring 127 .
  • the switching gate 123 and the side walls 129a and 129b for the storage spaces 130a and 130b form a single injection molded part 130 .
  • the striking pins 133a and 133b which are used to ignite one ignition unit 134a and 134b , are constantly under the pressure of a spring 135a and 135b .
  • the striking pins 133a and 133b are therefore already biased in the idle state.
  • the two striking pins 133a and 133b are held in the tensioned position in a trough 141a and 141b , respectively, by a locking slide 140a and 140b , which is provided with a through hole 137a and 137b and can be displaced perpendicularly to the axis 139a and 139b of each striking pin 133a and 133b .
  • a secure locking is given by the pressure of the spring 135a or 135b .
  • the self-defense device 120 is also secured against falling.
  • the low weight of each locking slide 140a or 140b is not sufficient to cause displacement when the device 120 hits the ground hard.
  • the end of the resilient arm 125a in the guide groove 144a of the shift gate 123 moves to the location 145a and the resilient arm 125b in the guide groove 144b to the location 145b .
  • the end of the resilient arm 125b does not pass the passage 146 .
  • the resilient arm 125a sweeps past a projection 148a of the locking slide 140a and thereby presses the locking slide 140a in the direction of the arrow 147 , as a result of which the tensioned striking pin 133a strikes the ignition set 134a through the through hole 137a and ignites it.
  • the active ingredient of the storage unit 121a is now expelled.
  • the end of the resilient arm 125b moves through the passage 146 and then remains at the location 149 .
  • the operating slide 124 therefore no longer slides completely back into its starting position in the case shown here. This incomplete decline indicates that a storage unit has already been fired. If the operating slide 124 is now pressed in a second time, the end of the spring arm 125b slides along the groove 150 , whereupon the projection 148b of the locking slide 140b is pressed in and the striking pin 133b is released for the ignition of the ignition unit 134b .
  • a pot-like housing 152a and 152b at the end of each storage unit 121a and 121b accommodates one of the striking springs 135a and 135b , a locking slide 140a and 140b , an ignition kit 134a and 134b and the associated propellant charge 151a and 151b .
  • These housings 152a and 152b serve as wall reinforcement in the rear area of the storage units 121a and 121b , where the highest pressure peaks arise during "firing".
  • the walls of the housings 152a and 152b are firmly connected to the ends of the storage units 121a and 121b by vibration welding .
  • the trigger mechanism shown here is rotating compared to the previous ones working easier trained and thus cheaper to manufacture.
  • the self-defense device 120 is made almost entirely of plastic. Only the pyrotechnic elements, which hold the propellant and the primer 134a / 151a or 134b / 151b , consist of brass components . When assembling the self-defense device 120 , the propellant and the primer 134a / 151a or 134b / 151b must not be heated above 100 ° C. Pouring into the plastic is therefore not possible because it is injected at a higher temperature. The ignition and the propellant charge 134a / 151a or 134b / 151b as well as the locking slides 140a and 140b together with the housings 152a and 152b receiving the prestressed striker pin 133a or 133b are thus only used later. The plastic parts are then joined together in a "cold" manner by means of vibration welding.
  • the storage units 1a, 1b, 91a and 91b can also be made significantly larger in their mechanical dimensions. If water or another fire-fighting agent is then used as the active substance, such storage units can be used together with a smoke or heat detector for automatic fire-fighting. Portable fire-fighting devices with several such storage units could also be manufactured.

Landscapes

  • General Engineering & Computer Science (AREA)
  • Engineering & Computer Science (AREA)
  • Burglar Alarm Systems (AREA)
  • Telephone Function (AREA)
  • Non-Silver Salt Photosensitive Materials And Non-Silver Salt Photography (AREA)
  • Toys (AREA)
  • Infusion, Injection, And Reservoir Apparatuses (AREA)
  • Electrotherapy Devices (AREA)
  • Nozzles (AREA)
  • Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
  • External Artificial Organs (AREA)
  • Catching Or Destruction (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Medicinal Preparation (AREA)
  • Portable Nailing Machines And Staplers (AREA)
EP00810459A 2000-05-26 2000-05-26 Conteneur pour un fluide susceptible d'être dispersé dans l'air libre et dispositif de défense comportant un tel conteneur Withdrawn EP1158263A1 (fr)

Priority Applications (15)

Application Number Priority Date Filing Date Title
EP00810459A EP1158263A1 (fr) 2000-05-26 2000-05-26 Conteneur pour un fluide susceptible d'être dispersé dans l'air libre et dispositif de défense comportant un tel conteneur
DE50109382T DE50109382D1 (de) 2000-05-26 2001-05-23 Abwehrvorrichtung, vorzugsweise selbstverteidigungsvorrichtung und eine hierin verwendbare speichereinheit
US10/296,399 US6951070B2 (en) 2000-05-26 2001-05-23 Defense device, preferably self-defense device and storage unit used therein
RU2002135081/02A RU2269082C2 (ru) 2000-05-26 2001-05-23 Оборонительное устройство, преимущественно устройство самозащиты, и используемый в нем патрон
CZ20023564A CZ20023564A3 (cs) 2000-05-26 2001-05-23 Obranné zařízení, zejména zařízení pro sebeobranu, a v něm použitelná zásobníková jednotka
CNB018132669A CN1205456C (zh) 2000-05-26 2001-05-23 防御装置,尤其是自卫装置和可用在该装置内的存储单元
BRPI0111178-7A BR0111178B1 (pt) 2000-05-26 2001-05-23 unidade de reservatório; tanque de carga substituìvel; unidade básica; e dispositivo de defesa.
PCT/CH2001/000319 WO2001090674A1 (fr) 2000-05-26 2001-05-23 Dispositif de defense, de preference dispositif d'autodefense, et ensemble reservoir utilisable dans un tel dispositif
AT01929163T ATE321989T1 (de) 2000-05-26 2001-05-23 Abwehrvorrichtung, vorzugsweise selbstverteidigungsvorrichtung und eine hierin verwendbare speichereinheit
KR1020027015967A KR20030005400A (ko) 2000-05-26 2001-05-23 방어 장치, 바람직하게는 호신 장치 및 이들에 사용되는저장 유닛
EP01929163A EP1285217B1 (fr) 2000-05-26 2001-05-23 Dispositif de defense, de preference dispositif d'autodefense, et ensemble reservoir utilisable dans un tel dispositif
AU2001256047A AU2001256047A1 (en) 2000-05-26 2001-05-23 Defense device, preferably self-defense device and storage unit used therein
IL15304201A IL153042A0 (en) 2000-05-26 2001-05-23 Defense device, preferably self-defense device and storage unit used therein
ZA200209603A ZA200209603B (en) 2000-05-26 2002-11-26 Defense device, preferably self-defense device and storage unit used therein.
US11/208,514 US7316090B2 (en) 2000-05-26 2005-08-23 Defense device, preferably self-defense device and storage unit used therein

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP00810459A EP1158263A1 (fr) 2000-05-26 2000-05-26 Conteneur pour un fluide susceptible d'être dispersé dans l'air libre et dispositif de défense comportant un tel conteneur

Publications (1)

Publication Number Publication Date
EP1158263A1 true EP1158263A1 (fr) 2001-11-28

Family

ID=8174724

Family Applications (2)

Application Number Title Priority Date Filing Date
EP00810459A Withdrawn EP1158263A1 (fr) 2000-05-26 2000-05-26 Conteneur pour un fluide susceptible d'être dispersé dans l'air libre et dispositif de défense comportant un tel conteneur
EP01929163A Expired - Lifetime EP1285217B1 (fr) 2000-05-26 2001-05-23 Dispositif de defense, de preference dispositif d'autodefense, et ensemble reservoir utilisable dans un tel dispositif

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP01929163A Expired - Lifetime EP1285217B1 (fr) 2000-05-26 2001-05-23 Dispositif de defense, de preference dispositif d'autodefense, et ensemble reservoir utilisable dans un tel dispositif

Country Status (13)

Country Link
US (2) US6951070B2 (fr)
EP (2) EP1158263A1 (fr)
KR (1) KR20030005400A (fr)
CN (1) CN1205456C (fr)
AT (1) ATE321989T1 (fr)
AU (1) AU2001256047A1 (fr)
BR (1) BR0111178B1 (fr)
CZ (1) CZ20023564A3 (fr)
DE (1) DE50109382D1 (fr)
IL (1) IL153042A0 (fr)
RU (1) RU2269082C2 (fr)
WO (1) WO2001090674A1 (fr)
ZA (1) ZA200209603B (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003042623A1 (fr) 2001-11-16 2003-05-22 Piexon Ag Dispositif comportant un reservoir rempli ou pouvant etre rempli d'un agent actif et une unite d'atomisation
WO2003054473A1 (fr) 2001-12-10 2003-07-03 Piexon Ag Dispositif de tir tenu a une main, comprenant plusieurs cartouches
ITPD20130302A1 (it) * 2013-11-08 2015-05-09 Alberto Pauletto Anello anti aggressione

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10150636C2 (de) * 2001-10-12 2003-08-21 Diehl Munitionssysteme Gmbh Hochspannungs-Generator, insbesondere zum Einsatz als Störfrequenz-Generator
DE10204266A1 (de) * 2002-02-02 2003-08-28 Fraunhofer Ges Forschung Selbstverteidigungsmodul und dessen Verwendung
GB0225597D0 (en) * 2002-11-02 2002-12-11 Fluiditi Ltd Fluid delivery system
US20070006506A1 (en) * 2005-07-08 2007-01-11 Mey-Chu Lan Liquid filling bullet for physical protection
US20070158463A1 (en) * 2006-01-04 2007-07-12 Mey-Chu Lan Liquid spraying device with return-preventing structure
WO2008006249A1 (fr) * 2006-07-07 2008-01-17 Sichuan Nanshan Power Actuated Fastening System Co., Ltd Unité d'éjection de liquide
KR101046885B1 (ko) * 2009-04-10 2011-07-06 최현정 단말기용 액 분사장치
JP5449922B2 (ja) * 2009-05-11 2014-03-19 日本工機株式会社 携帯型液体噴射装置
KR200452397Y1 (ko) * 2009-08-27 2011-02-28 채준수 바늘볼을 이용한 휴대용 호신용구
US9277748B2 (en) * 2010-03-12 2016-03-08 The United States Of America, As Represented By The Secretary, Department Of Health & Human Services Agonist/antagonist compositions and methods of use
US8534174B2 (en) * 2010-09-27 2013-09-17 Power Tool Institute Pyrotechnic actuator and power cutting tool with safety reaction system having such pyrotechnic actuator
US9182198B2 (en) * 2012-05-29 2015-11-10 Fosol, Llc Wearable personal protection device with safety mechanism
CN102728505B (zh) * 2012-06-12 2014-08-06 许杭旭 一种喷泉用气压喷头
US9468305B2 (en) * 2014-07-24 2016-10-18 Iqbal Singh Flora Folding bed for space saving storage within a cabinet
US9791247B2 (en) 2015-05-12 2017-10-17 Cgs Group Llc Firing device
CN106628158A (zh) * 2017-02-28 2017-05-10 罗熠 一种防暴无人机
RU2673829C1 (ru) * 2017-03-14 2018-11-30 Семен Валентинович Гусев Оружейный модуль и картридж специального назначения
US11022406B2 (en) 2018-11-06 2021-06-01 Adrian Rice Inconspicuous defense substance spray canister
DE102019105161A1 (de) * 2019-02-28 2020-09-03 Carl Hoernecke Chem. Fabrik Gmbh & Co. Kg Reizstoffkartusche sowie Reizstoff-Sprühgerät
US11320233B2 (en) 2019-10-10 2022-05-03 Hero Defense Systems, LLC Non-lethal self-protection system
RU200476U1 (ru) * 2020-06-26 2020-10-27 ПАО "Кировский завод "Маяк" Баллончик аэрозольный малогабаритный
US11519700B2 (en) * 2020-11-30 2022-12-06 Hero Defense Systems, LLC Non-lethal self-protection weapon
USD995703S1 (en) 2021-11-04 2023-08-15 Hero Defense Systems, LLC Gripless non-lethal personal-defense weapon
CN114812269B (zh) * 2022-03-10 2023-04-07 江苏世安警用装备有限公司 一种主动防卫警用高速催泪枪

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1741902A (en) 1928-04-27 1929-12-31 Reginald J Alden Firearm
DE601764C (de) * 1931-08-14 1934-08-23 Richard Brunar Gasdruckzerstaeuber fuer Fluessigkeiten zur Schaedlingsbekaempfung
FR776954A (fr) 1933-10-25 1935-02-08 Arme défensive
US2432791A (en) * 1945-12-12 1947-12-16 Osses Jacob Defense weapon
GB937023A (en) * 1962-04-19 1963-09-18 Aerojet General Co Fluid projection apparatus
US3335722A (en) 1963-11-01 1967-08-15 Olin Mathieson Hypodermic device
US3802430A (en) 1972-06-30 1974-04-09 L Arnold Disposable pyrotechnically powered injector
US4089334A (en) 1976-10-07 1978-05-16 Schwebel Paul R Pyrotechnically powered needleless injector
US4124024A (en) 1977-03-03 1978-11-07 Schwebel Paul R Disposable hypodermic injection ampule
DE3310155A1 (de) 1983-03-21 1984-09-27 Adam 6114 Groß-Umstadt Merkel Handschuh-gas-pistole-kaliber 8 m/m
DE19624582A1 (de) * 1996-06-20 1998-01-02 Peter Dipl Ing Dr Lell Flüssigkeitszerstäuber
WO1998038468A1 (fr) 1997-02-25 1998-09-03 Tchorbadjiiska, Yuolka Ilieva Pistolet camoufle a double canon
WO2000006965A1 (fr) * 1998-07-27 2000-02-10 Thomann Juerg Systeme d'autodefense

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE310155C (fr)
US17813A (en) * 1857-07-14 Machine for cutting metal
US1598784A (en) * 1926-02-17 1926-09-07 Fed Lab Inc Hand weapon
USRE17813E (en) * 1928-09-13 1930-09-23 Pistol
US1947834A (en) * 1931-09-19 1934-02-20 Jr Louis L Driggs Flare signal
US2829595A (en) * 1951-11-23 1958-04-08 Olin Mathieson Shot shells
US3127836A (en) * 1962-04-24 1964-04-07 Olin Mathieson Abattoir device
US3315397A (en) * 1965-11-29 1967-04-25 Clarence W Gilliam Flare gun having quick disconnect coupling
US3431853A (en) * 1966-01-06 1969-03-11 Albert C Warner Defensive weapon and cartridge therefor
US3507220A (en) * 1969-01-02 1970-04-21 Clifton M Mcclure Ammunition round
US3706151A (en) * 1970-05-01 1972-12-19 Robert M Mcneill Gun and projectile for shooting fluids
DE3235013C2 (de) * 1982-09-22 1986-03-06 Wilhelm Meyer oHG, 8500 Nürnberg Handfeuerschußvorrichtung
US5318492A (en) * 1993-02-05 1994-06-07 Quinn Joan M Jogging weight with repellent chemical
US5952601A (en) * 1998-04-23 1999-09-14 The United States Of America As Represented By The Secretary Of The Navy Recoilless and gas-free projectile propulsion

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1741902A (en) 1928-04-27 1929-12-31 Reginald J Alden Firearm
DE601764C (de) * 1931-08-14 1934-08-23 Richard Brunar Gasdruckzerstaeuber fuer Fluessigkeiten zur Schaedlingsbekaempfung
FR776954A (fr) 1933-10-25 1935-02-08 Arme défensive
US2432791A (en) * 1945-12-12 1947-12-16 Osses Jacob Defense weapon
GB937023A (en) * 1962-04-19 1963-09-18 Aerojet General Co Fluid projection apparatus
US3335722A (en) 1963-11-01 1967-08-15 Olin Mathieson Hypodermic device
US3802430A (en) 1972-06-30 1974-04-09 L Arnold Disposable pyrotechnically powered injector
US4089334A (en) 1976-10-07 1978-05-16 Schwebel Paul R Pyrotechnically powered needleless injector
US4124024A (en) 1977-03-03 1978-11-07 Schwebel Paul R Disposable hypodermic injection ampule
DE3310155A1 (de) 1983-03-21 1984-09-27 Adam 6114 Groß-Umstadt Merkel Handschuh-gas-pistole-kaliber 8 m/m
DE19624582A1 (de) * 1996-06-20 1998-01-02 Peter Dipl Ing Dr Lell Flüssigkeitszerstäuber
WO1998038468A1 (fr) 1997-02-25 1998-09-03 Tchorbadjiiska, Yuolka Ilieva Pistolet camoufle a double canon
WO2000006965A1 (fr) * 1998-07-27 2000-02-10 Thomann Juerg Systeme d'autodefense

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003042623A1 (fr) 2001-11-16 2003-05-22 Piexon Ag Dispositif comportant un reservoir rempli ou pouvant etre rempli d'un agent actif et une unite d'atomisation
WO2003054473A1 (fr) 2001-12-10 2003-07-03 Piexon Ag Dispositif de tir tenu a une main, comprenant plusieurs cartouches
ITPD20130302A1 (it) * 2013-11-08 2015-05-09 Alberto Pauletto Anello anti aggressione

Also Published As

Publication number Publication date
US7316090B2 (en) 2008-01-08
US20040020946A1 (en) 2004-02-05
US6951070B2 (en) 2005-10-04
RU2269082C2 (ru) 2006-01-27
CN1444720A (zh) 2003-09-24
EP1285217A1 (fr) 2003-02-26
CZ20023564A3 (cs) 2003-05-14
ZA200209603B (en) 2003-11-26
CN1205456C (zh) 2005-06-08
BR0111178A (pt) 2003-06-10
ATE321989T1 (de) 2006-04-15
KR20030005400A (ko) 2003-01-17
US20060010745A1 (en) 2006-01-19
BR0111178B1 (pt) 2010-06-29
EP1285217B1 (fr) 2006-03-29
IL153042A0 (en) 2003-06-24
WO2001090674A1 (fr) 2001-11-29
AU2001256047A1 (en) 2001-12-03
DE50109382D1 (de) 2006-05-18

Similar Documents

Publication Publication Date Title
EP1285217B1 (fr) Dispositif de defense, de preference dispositif d'autodefense, et ensemble reservoir utilisable dans un tel dispositif
DE69512118T2 (de) Geschoss, insbesondere nicht tötende Patrone
DE19944486C2 (de) Irritationskörper
EP1451519B1 (fr) Dispositif de tir tenu a une main, comprenant plusieurs cartouches
EP1312888B1 (fr) Dispositif avec réservoir pour agent chimique et atomiseur
DE10303106B4 (de) Barrikadenbrecher
DE4447470B4 (de) Infrarotköderpatrone
DE69810879T2 (de) Projektil mit radialer Wirkrichtung
DE69613034T2 (de) Nichtletale Munition mit einem unschädlichmachenden Effekt
DE69608644T2 (de) Dispersions- oder Auftragungsverfahren eines aktiven Materials, Zusammensetzung und Gemäss diesem Verfahren hergestelltes Geschoss
DE3919314A1 (de) Zerlegergeschoss
DE69106322T2 (de) Gewehrgranate.
DE3040721C1 (de) Geschoß
DE2234302C3 (fr)
WO2014180766A1 (fr) Projectile, notamment à lancer à la main
DE2648014A1 (de) Wurf- oder gewehrgeschoss
DE375142C (de) Bombe mit einer in das Innere eines kurzen Rohres einer Schleuderwaffe einzufuehrenden Huelse
DE2352576A1 (de) Vorrichtung zur zuendueberfuehrung fuer geschosse mit hinauswerfbaren koerpern
EP0594035B1 (fr) Procédé et dispositif pour combattre les insects
CH679243A5 (en) Self-loading pistol - has electronic and mechanical firing systems
DE2042000A1 (de) Spuranzeigendes Ausbildungsgeschoss mit Rauchanzeige und Eigenzerstoerung
DE1728283C2 (de) Geschoß zur Beschädigung oder Zerstörung von Flugkörpern bzw. deren Triebwerken
DE10359287A1 (de) Vorrichtung zum Ausstoßen von Wirkstoffkörpen, insbondere Reizstoffkörpern
AT229195B (de) Zünder für rotierende Geschosse
DE2234302B2 (de) Rakete

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

AX Request for extension of the european patent

Free format text: AL;LT;LV;MK;RO;SI

AKX Designation fees paid
REG Reference to a national code

Ref country code: DE

Ref legal event code: 8566

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20020529