EP1716385B1 - An electropyrotechnic initiator with heat dissipation - Google Patents
An electropyrotechnic initiator with heat dissipation Download PDFInfo
- Publication number
- EP1716385B1 EP1716385B1 EP05707343A EP05707343A EP1716385B1 EP 1716385 B1 EP1716385 B1 EP 1716385B1 EP 05707343 A EP05707343 A EP 05707343A EP 05707343 A EP05707343 A EP 05707343A EP 1716385 B1 EP1716385 B1 EP 1716385B1
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- EP
- European Patent Office
- Prior art keywords
- heat
- resistor element
- heater resistor
- heat dissipator
- support
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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- 239000003999 initiator Substances 0.000 title claims abstract description 36
- 230000017525 heat dissipation Effects 0.000 title 1
- 229910052751 metal Inorganic materials 0.000 claims abstract description 11
- 239000002184 metal Substances 0.000 claims abstract description 11
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 8
- 229910052802 copper Inorganic materials 0.000 claims abstract description 8
- 239000010949 copper Substances 0.000 claims abstract description 8
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 6
- 239000000956 alloy Substances 0.000 claims abstract description 6
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 5
- 230000005611 electricity Effects 0.000 claims abstract description 4
- 239000000853 adhesive Substances 0.000 claims description 13
- 230000001070 adhesive effect Effects 0.000 claims description 13
- 239000000463 material Substances 0.000 claims description 3
- 229910010293 ceramic material Inorganic materials 0.000 claims description 2
- 239000007769 metal material Substances 0.000 claims description 2
- 238000010438 heat treatment Methods 0.000 abstract description 4
- 239000000919 ceramic Substances 0.000 abstract 1
- 239000000615 nonconductor Substances 0.000 abstract 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 9
- 229910052726 zirconium Inorganic materials 0.000 description 9
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 8
- 239000000203 mixture Substances 0.000 description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 7
- 239000000758 substrate Substances 0.000 description 7
- 239000010936 titanium Substances 0.000 description 7
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- 238000010304 firing Methods 0.000 description 4
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- 239000000377 silicon dioxide Substances 0.000 description 4
- 235000012239 silicon dioxide Nutrition 0.000 description 4
- 229910052719 titanium Inorganic materials 0.000 description 4
- 239000002131 composite material Substances 0.000 description 3
- 239000011521 glass Substances 0.000 description 3
- 230000000977 initiatory effect Effects 0.000 description 3
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- 239000000843 powder Substances 0.000 description 3
- 239000004593 Epoxy Substances 0.000 description 2
- AXZAYXJCENRGIM-UHFFFAOYSA-J dipotassium;tetrabromoplatinum(2-) Chemical compound [K+].[K+].[Br-].[Br-].[Br-].[Br-].[Pt+2] AXZAYXJCENRGIM-UHFFFAOYSA-J 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- -1 polyethylene terephthalate Polymers 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- FGIUAXJPYTZDNR-UHFFFAOYSA-N potassium nitrate Chemical compound [K+].[O-][N+]([O-])=O FGIUAXJPYTZDNR-UHFFFAOYSA-N 0.000 description 2
- 229910001487 potassium perchlorate Inorganic materials 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000001052 transient effect Effects 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 229910001006 Constantan Inorganic materials 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 239000000020 Nitrocellulose Substances 0.000 description 1
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- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000003213 activating effect Effects 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 239000000788 chromium alloy Substances 0.000 description 1
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- 150000001875 compounds Chemical class 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
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- WETZJIOEDGMBMA-UHFFFAOYSA-L lead styphnate Chemical compound [Pb+2].[O-]C1=C([N+]([O-])=O)C=C([N+]([O-])=O)C([O-])=C1[N+]([O-])=O WETZJIOEDGMBMA-UHFFFAOYSA-L 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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- 229910001120 nichrome Inorganic materials 0.000 description 1
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- 229920001220 nitrocellulos Polymers 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- 229920000139 polyethylene terephthalate Polymers 0.000 description 1
- 239000005020 polyethylene terephthalate Substances 0.000 description 1
- 235000010333 potassium nitrate Nutrition 0.000 description 1
- 239000004323 potassium nitrate Substances 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229920005992 thermoplastic resin Polymers 0.000 description 1
- 229910000048 titanium hydride Inorganic materials 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
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Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B3/00—Blasting cartridges, i.e. case and explosive
- F42B3/10—Initiators therefor
- F42B3/103—Mounting initiator heads in initiators; Sealing-plugs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B3/00—Blasting cartridges, i.e. case and explosive
- F42B3/10—Initiators therefor
- F42B3/12—Bridge initiators
- F42B3/124—Bridge initiators characterised by the configuration or material of the bridge
Definitions
- the invention relates to an electropyrotechnic initiator.
- the field of application of the invention relates to initiators for firing the pyrotechnic charges of gas generators for activating devices for protecting the occupants of motor vehicles, such as, for example, air bags.
- such an initiator comprises a pyrotechnic ignition charge and a heater resistor element covered by the pyrotechnic ignition charge to ignite it by the Joule effect.
- Two electrodes are provided for being fed with electricity.
- electropyrotechnic initiators is influenced by the pair constituted by the resistor element and the ignition pyrotechnic charge, and by the sensitivity imparted to such initiators by the pair used.
- the all-fire threshold corresponds to the limit value for electrical current passing via the electrodes, above which it is certain that the initiator will function, i.e. that the ignition pyrotechnic charge will ignite.
- the no-fire threshold corresponds to the limiting value for electrical current passing via the electrodes, below which it is certain that the initiator will not function, i.e. that the ignition pyrotechnic charge will not ignite.
- Document US-A-6 272 965 concerns an electro-explosive device ("EED") having resistors fabricated on a thermally conductive substrate and interconnected by a central bridge element.
- the resistance of the bridge element is lower than that of the resistors, which have a larger surface area to volume ratio.
- a layer of zirconium is placed on the bridge element and explodes into a plasma along with the bridge element in order to ignite a pyrotechnic compound.
- the substrate using integrated circuit fabrication techniques and the conductive bridge of the EED is overcoated with a composite overcoat comprising a metal and an oxidizer, which produces a chemical explosion upon plasma vaporization of the conductive bridge.
- the EED comprises a silicon wafer, or a thermally conductive but electrically insulating substrate, such as alumina, which has layers of silicon dioxide grown on the front and back surfaces.
- the silicon dioxide layers electrically insulate the substrate while providing a low thermal path of resistance across the front and back surfaces of the substrate.
- the substrate has a nominal low resistivity.
- a layer of titanium is vapor deposited onto the front surface followed by a layer of zirconium. The zirconium/titanium layer is then selectively etched away to form a bowtie pattern having a central bridge portion.
- a layer of titanium/nickel/gold is deposited over the back layer of silicon dioxide and Ti/Ni/Au layers are also deposited over the ends of the bowtie shaped zirconium layer to form contact pads.
- the resistance of the EED is comprised of three resistors in series, with Rland being the resistance through the Ti/Ni/Au layers to either end of the bowtie-shaped zirconium layer and Rbow being the resistance of the bowtie-shaped zirconium layer. With low levels of input signals, the resistances Rland have a much larger surface to volume ratio than the resistance Rbow. Thus, at these levels, the resistances Rland receive most of the energy from the input signals and convert the energy into heat.
- the Ti/Ni/Au contacts present a large surface area for the conduction of heat through the top silicon dioxide layer, through the thermally conductive substrate and to the header.
- the zirconium-shaped bowtie dissipates only a fraction of the heat and remains relatively cool.
- the EED is ignited by supplying a firing signal which has a relatively high intensity.
- the resistances Rland comprise metal-oxide variable resistances which are formed between the titanium layer in contacts and an oxide-phase layer formed on the zirconium layer.
- the metal-oxide variable resistances Rland have a relatively high resistance at lower voltages.
- the metal-oxide resistances Rland decrease substantially and become small in comparison to the resistance Rbow.
- the resistance Rbow will become the largest resistance and will accordingly receive most of the energy from the firing signal until the zirconium layer vaporizes in a plasma.
- the container 2 is made of thin light metal, e.g. aluminum, and its plane wall 8 is advantageously weakened so as to open easily under the effect of an increase in the pressure that exists inside the container.
- the overmolding 6 is preferably made of a thermoplastic resin such as polyethylene terephthalate, for example.
- the body 3 is made out of a dense metal such as steel, for example.
- the body 3 presents a plane top face 9 and a likewise plane bottom face 15, and over its full height h, it encases an electrically-insulating structure through which there pass two electrically-conducting electrodes 12 and 13.
- This structure for passing the two electrodes 12 and 13 is vitreous, for example.
- the two electrodes 12 and 13 are in the form of pins, for example.
- this structure for passing the two electrodes 12 and 13 is formed by two hollow electrically-insulating tubes 10 and 11, e.g. made of glass, themselves encasing respective ones of the two electrodes 12 and 13.
- the structure for passing the two electrodes 12 and 13 could comprise a single tube 10 or 11 encasing the corresponding electrode 12 or 13.
- the body 3 could be electrically-insulating, and could itself encase the electrodes 12 and 13 directly without using tubes 10 and 11, with the body then being made of glass, for example.
- one of the electrodes 12, 13 surrounded by an electrically-insulating tube 10, 11 may be of the coaxial type, i.e. being electrically connected to the body 3 via a connection situated beneath it.
- a heat dissipator 31 is provided between the support 16 and the heater resistor element 17.
- This heat dissipator 31 is electrically insulated from the electrodes 12 and 13 and from the resistor element 17 by any appropriate means that also enables the heat produced by the heater resistor element 17 to be conducted towards the heat dissipator 31.
- the heat dissipator 31 does not touch the heater resistor element 17.
- the heat dissipator 31 conducts heat and serves to dissipate the heat produced by the heater resistor element 17 towards the support 16.
- the heat dissipator presents thermal conductivity greater than or equal to 100 milliwatts per centimeter per Kelvin (mW/cm.K) (which applies to Constantan, being the least thermally conductive of copper-based alloys), and is preferably greater than or equal to 200 mW/cm.K.
- mW/cm.K milliwatts per centimeter per Kelvin
- the heat dissipator 31 is constituted, for example, by a heat-conducting layer 31 of determined and continuous thickness, as shown in Figures 2 and 3 .
- the heat dissipator 31 is electrically conductive, e.g. being made of metal, such as copper or aluminum. Naturally, any other heat conducting material could be used for the heat dissipator 31.
- a second layer 33 of heat-conducting and electrically-insulating adhesive is interposed between the heat dissipator 31 and the support 16.
- the layer 33 of adhesive provides physical contact between the dissipator 31 and the support 16.
- the first and second layers 32 and 33 surround all sides of the heat dissipator 31 between the support 16, the heater resistor element 17, and the channels 22, 23 for passing the electrodes 12, 13, meeting each other between each channel 22, 23 and the thickness of the heat dissipator 31, so that the heat dissipator 31 is then embedded in the first and second layers 32 and 33.
- the first and second layers 32 and 33 meet around the channels 22 and 23 where they provide support for the electrically-conducting layer 25.
- the second layer 33 of adhesive is omitted beneath the heat dissipator 31, and the heat dissipator 31 is in direct contact with the support 16.
- the heat dissipator 31 is positioned in the desired location on the support 16 which has a plane top surface, and the layer 32 of adhesives followed by the circuit 18 are then deposited on the heat dissipator 31 and the support 16.
- the first layer 32 of adhesive surrounds the top and the sides of the heat dissipator 31 between the support 16, the heater resistor element 17, and the channels 22 and 23 for passing the electrodes 12 and 13, and meets between each channel 22, 23 and the heat dissipator 31 the support 16.
- the first layer 32 surrounds the channels 22 and 23 where it acts as a support for the electrically-conducting layer 25.
- the dissipator 31 may be inserted in part in the thickness direction in a corresponding recess in the support 16, so that its bottom surface 34 and a fraction of its flanks 35 come into contact with the recess in the support 16, as shown in Figure 4 .
- the presence of the heat dissipator 31 enables the value of the no-fire threshold to be set and raised so as to reduce the difference between the no-fire threshold and the all-fire threshold, as shown in the table below, where the no-fire current and the all-fire current are given with reliability of 99.9%, the element 17 being made of NiCr, and where the no-fire current is raised by more than 44% by the presence of the dissipator. This makes the operation of the initiator more reliable. Initiator No-fire current in mA (10 s/+90°C) All-fire current in mA (2 ms/-40°C) With heat dissipator (17 micrometer thick copper layer) 551 1005 Without heat dissipator 381 998
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Resistance Heating (AREA)
- Air Bags (AREA)
- Thermally Actuated Switches (AREA)
Abstract
Description
- The invention relates to an electropyrotechnic initiator.
- The field of application of the invention relates to initiators for firing the pyrotechnic charges of gas generators for activating devices for protecting the occupants of motor vehicles, such as, for example, air bags.
- Usually, such an initiator comprises a pyrotechnic ignition charge and a heater resistor element covered by the pyrotechnic ignition charge to ignite it by the Joule effect. Two electrodes are provided for being fed with electricity.
- The operation of electropyrotechnic initiators is influenced by the pair constituted by the resistor element and the ignition pyrotechnic charge, and by the sensitivity imparted to such initiators by the pair used.
- Thus, the all-fire threshold corresponds to the limit value for electrical current passing via the electrodes, above which it is certain that the initiator will function, i.e. that the ignition pyrotechnic charge will ignite.
- The no-fire threshold, lower than the all-fire threshold, corresponds to the limiting value for electrical current passing via the electrodes, below which it is certain that the initiator will not function, i.e. that the ignition pyrotechnic charge will not ignite.
- Between the no-fire threshold and the all-fire threshold, there exists a transient zone in which it is not certain whether the initiator will or will not function.
- Document
US-A-6 272 965 concerns an electro-explosive device ("EED") having resistors fabricated on a thermally conductive substrate and interconnected by a central bridge element. The resistance of the bridge element is lower than that of the resistors, which have a larger surface area to volume ratio. A layer of zirconium is placed on the bridge element and explodes into a plasma along with the bridge element in order to ignite a pyrotechnic compound. The substrate using integrated circuit fabrication techniques and the conductive bridge of the EED is overcoated with a composite overcoat comprising a metal and an oxidizer, which produces a chemical explosion upon plasma vaporization of the conductive bridge. In the second embodiment of this document, the EED comprises a silicon wafer, or a thermally conductive but electrically insulating substrate, such as alumina, which has layers of silicon dioxide grown on the front and back surfaces. The silicon dioxide layers electrically insulate the substrate while providing a low thermal path of resistance across the front and back surfaces of the substrate. Preferably, the substrate has a nominal low resistivity. A layer of titanium is vapor deposited onto the front surface followed by a layer of zirconium. The zirconium/titanium layer is then selectively etched away to form a bowtie pattern having a central bridge portion. A layer of titanium/nickel/gold is deposited over the back layer of silicon dioxide and Ti/Ni/Au layers are also deposited over the ends of the bowtie shaped zirconium layer to form contact pads. The resistance of the EED is comprised of three resistors in series, with Rland being the resistance through the Ti/Ni/Au layers to either end of the bowtie-shaped zirconium layer and Rbow being the resistance of the bowtie-shaped zirconium layer. With low levels of input signals, the resistances Rland have a much larger surface to volume ratio than the resistance Rbow. Thus, at these levels, the resistances Rland receive most of the energy from the input signals and convert the energy into heat. The Ti/Ni/Au contacts present a large surface area for the conduction of heat through the top silicon dioxide layer, through the thermally conductive substrate and to the header. As a result, at low levels of input signal, the zirconium-shaped bowtie dissipates only a fraction of the heat and remains relatively cool. Thus, the EED can remain insensitive to any RF power or ESD which is coupled to the EED. The EED is ignited by supplying a firing signal which has a relatively high intensity. The resistances Rland comprise metal-oxide variable resistances which are formed between the titanium layer in contacts and an oxide-phase layer formed on the zirconium layer. The metal-oxide variable resistances Rland have a relatively high resistance at lower voltages. With higher intensity signals, the metal-oxide resistances Rland decrease substantially and become small in comparison to the resistance Rbow. As a result, with a high intensity firing signal, the resistance Rbow will become the largest resistance and will accordingly receive most of the energy from the firing signal until the zirconium layer vaporizes in a plasma. - The invention seeks to obtain an electropyrotechnic initiator serving to reduce the range of uncertainty concerning the functioning of electropyrotechnic initiators between the no-fire threshold and the all-fire threshold.
- To this end, in a first aspect, the invention provides an electropyrotechnic initiator according to claim 1.
- By means of the invention, a fraction of the heat produced by the heater resistor element in operation of the initiator is dissipated towards the support. The no-fire threshold value is thus raised towards the all-fire threshold, thereby reducing the transient zone between them. The value of the no-fire threshold is raised, while the value of the all-fire threshold remains substantially constant. Consequently, the initiator of the invention presents greater safety in operation and is more robust against stray electrical currents. Thus, the invention makes it possible to satisfy better the requirements laid down by motor vehicle manufacturers for the no-fire and all-fire thresholds.
- According to
claims 2 to 9 depending on claim 1: - a second layer of heat-conducting and electrically-insulating adhesive is interposed between the heat dissipator and the support;
- or the heat dissipator is in direct contact with the support;
- the heat dissipator is formed by a heat-conducting layer;
- the heat dissipator is made of a material selected from metal materials and ceramic materials;
- the heat dissipator is made of a metal selected from copper, aluminum, alloys thereof, or oxides thereof;
- the heat dissipator is located beneath the heater resistor element; and
- the heater resistor element is covered by two electrical contacts that are separate from each other and in contact with respective ones of the two electrodes.
- The invention will be better understood on reading the following description given purely by way of nonlimiting example and with reference to the accompanying drawings, in which:
-
Figure 1 is a diagrammatic axial vertical section of an initiator according to the invention; -
Figure 2 is a diagrammatic axial vertical section showing the disposition of the heater resistor element on the support in a first embodiment of the initiator according toFigure 1 ; -
Figure 3 is a diagrammatic axial vertical section showing the disposition of the heater resistor element on the support in a second embodiment of the initiator according toFigure 1 ; and -
Figure 4 is a diagrammatic axial vertical section showing the disposition of the heater resistor element on the support in a third embodiment of the initiator according toFigure 1 . - An electropyrotechnic initiator 1 according to the invention is shown in
Figure 1 . The initiator 1 comprises acylindrical container 2 that is circular about the vertical axis of the initiator, and that is also fragmentable and open at one of its ends. A solid circularcylindrical body 3 closes the open end of thecontainer 2. Theside wall 4 of thebody 3 presents anoutside shoulder 5 against which the open end of thecontainer 2 comes to bear. Thecontainer 2 and thebody 3 are encased in overmolding 6 that holds them together. Thecontainer 2 is thus in the form of a cylindrical cap presenting aside wall 7 and atop wall 8 which is plane, closed, and solid. By way of example, thecontainer 2 also contains ametal tube 20 reinforcing theside wall 7. Thecontainer 2 is made of thin light metal, e.g. aluminum, and itsplane wall 8 is advantageously weakened so as to open easily under the effect of an increase in the pressure that exists inside the container. The overmolding 6 is preferably made of a thermoplastic resin such as polyethylene terephthalate, for example. Thebody 3 is made out of a dense metal such as steel, for example. - The
body 3 presents a plane top face 9 and a likewiseplane bottom face 15, and over its full height h, it encases an electrically-insulating structure through which there pass two electrically-conducting 12 and 13. This structure for passing the twoelectrodes 12 and 13 is vitreous, for example. The twoelectrodes 12 and 13 are in the form of pins, for example. In the embodiment shown, this structure for passing the twoelectrodes 12 and 13 is formed by two hollow electrically-electrodes insulating tubes 10 and 11, e.g. made of glass, themselves encasing respective ones of the two 12 and 13. In a variant, the structure for passing the twoelectrodes 12 and 13 could comprise aelectrodes single tube 10 or 11 encasing the 12 or 13. In another variant, thecorresponding electrode body 3 could be electrically-insulating, and could itself encase the 12 and 13 directly without usingelectrodes tubes 10 and 11, with the body then being made of glass, for example. In an embodiment that is not shown, one of the 12, 13 surrounded by an electrically-insulatingelectrodes tube 10, 11 may be of the coaxial type, i.e. being electrically connected to thebody 3 via a connection situated beneath it. - The plane top face 9 of the
body 3 is fixed to asupport 16, e.g. by means of adhesive. In the embodiments shown as examples in the figures, thesupport 16 is isolated from the 12 and 13, is made of an electrically-insulating material, and is constituted, for example, by a board made of a glass/resin mixture, such as a composite polymer of the epoxy type filled with glass fibers. Two throughelectrodes 22 and 23 are provided in thecylindrical channels support 16 for passing the 12 and 13. Eachelectrodes 12, 13 presents a respectiveelectrode 12b, 13b which projects beyond the plane top face 9 of thetop end body 3 and that of thesupport 16, and a 12c, 13c which projects beyond thesecond end bottom face 14 of theovermolding 6. - The
support 16 carries anelectrical circuit 18 which includes aheater resistor element 17 or heatingresistive element 17 and which is electrically connected to the 12 and 13.electrodes - The
resistor element 17 is photoetched in conventional manner. Theresistor element 17 presents atop surface 24 which is covered by an ignition pyrotechnic charge contained in thecontainer 2, or in the embodiment shown, in thecontainer 2 and in themetal tube 20. This ignition pyrotechnic charge comprises, for example, an initiationpyrotechnic composition 19 which is in contact with theheater resistor element 17 and which is based, for example, on lead trinitroresorcinate, and an ignition composition orpowder 21 which covers the initiationpyrotechnic composition 19 and which is constituted, for example, by powder based on nitrocellulose or by a mixture of boron and of potassium nitrate. By way of example, theheater resistor element 17 is flat. As for the initiators in the table below, the initiationpyrotechnic composition 19 could also be a mixture of zirconium and of potassium perchlorate, and theignition powder 21 could be a mixture of titanium hydride and potassium perchlorate. - By way of example, the
heater resistor element 17 is made of metal and is formed, for example, by the middle portion of an electrically-conductinglayer 25, and for example a nickel/chromium alloy or some other alloy, e.g. a PtW alloy. Apart from its middle portion forming theheater resistor element 17, thelayer 25 is covered by two separate 26 and 27 making contact with the twoelectrical contacts 12 and 13 respectively. Theelectrodes 26 and 27 are covered by the ignition pyrotechnic charge, co-operate with thecontacts layer 25 to form theelectrical circuit 18 and comprise, for example, alayer 28 of copper on thelayer 25. This layer of copper is covered by another layer ofmetallization 29, for example. Thelayer 25 and the 26 and 27 outside thecontacts heater resistor element 17 have the 12 and 13 passing therethrough.electrodes - In
Figures 2 and 3 , aheat dissipator 31 is provided between thesupport 16 and theheater resistor element 17. Thisheat dissipator 31 is electrically insulated from the 12 and 13 and from theelectrodes resistor element 17 by any appropriate means that also enables the heat produced by theheater resistor element 17 to be conducted towards theheat dissipator 31. InFigures 2 and 3 , theheat dissipator 31 does not touch theheater resistor element 17. Theheat dissipator 31 conducts heat and serves to dissipate the heat produced by theheater resistor element 17 towards thesupport 16. By way of example, the heat dissipator presents thermal conductivity greater than or equal to 100 milliwatts per centimeter per Kelvin (mW/cm.K) (which applies to Constantan, being the least thermally conductive of copper-based alloys), and is preferably greater than or equal to 200 mW/cm.K. - The
heat dissipator 31 is either situated beneath theheater resistor element 17, e.g. in register therewith as shown by dashed lines inFigures 2 and 3 , or else it projects beyond said position beneath the 26 and 27, as shown by continuous lines incontacts Figures 2 and 3 . The figures are not to scale nor are ratios between dimensions complied with, and theheat dissipator 31 may extend beneath the resistor element by as much as the length of theheater resistor element 17 between the 26 and 27, or even more, for example. By way of example, thecontacts dissipator 31 may surround the 22, 23 and thechannels 12, 13, without touching them.pins - The
heat dissipator 31 is constituted, for example, by a heat-conductinglayer 31 of determined and continuous thickness, as shown inFigures 2 and 3 . By way of example, theheat dissipator 31 is electrically conductive, e.g. being made of metal, such as copper or aluminum. Naturally, any other heat conducting material could be used for theheat dissipator 31. - In the embodiments shown in
Figures 2 and 3 , in order to insulate theheat dissipator 31 electrically from theheater resistor element 17, afirst layer 32 of heat-conducting and electrically-insulating adhesive is interposed between theheater resistor element 17 and theheat dissipator 31. Thelayer 32 of adhesive provides physical contact between theheater element 17 and thedissipator 31. Thelayer 32 of adhesive is of thickness between theheater resistor element 17 and theheat dissipator 31 that is less than half the total thickness of thelayer 32 of adhesive between thecircuit 18 and thesupport 16. - In the embodiment shown in
Figure 2 , asecond layer 33 of heat-conducting and electrically-insulating adhesive is interposed between theheat dissipator 31 and thesupport 16. Thelayer 33 of adhesive provides physical contact between the dissipator 31 and thesupport 16. By way of example, the first and 32 and 33 surround all sides of thesecond layers heat dissipator 31 between thesupport 16, theheater resistor element 17, and the 22, 23 for passing thechannels 12, 13, meeting each other between eachelectrodes 22, 23 and the thickness of thechannel heat dissipator 31, so that theheat dissipator 31 is then embedded in the first and 32 and 33. The first andsecond layers 32 and 33 meet around thesecond layers 22 and 23 where they provide support for the electrically-conductingchannels layer 25. - In the embodiment shown in
Figure 3 , thesecond layer 33 of adhesive is omitted beneath theheat dissipator 31, and theheat dissipator 31 is in direct contact with thesupport 16. To do this, theheat dissipator 31 is positioned in the desired location on thesupport 16 which has a plane top surface, and thelayer 32 of adhesives followed by thecircuit 18 are then deposited on theheat dissipator 31 and thesupport 16. Thefirst layer 32 of adhesive surrounds the top and the sides of theheat dissipator 31 between thesupport 16, theheater resistor element 17, and the 22 and 23 for passing thechannels 12 and 13, and meets between eachelectrodes 22, 23 and thechannel heat dissipator 31 thesupport 16. Thefirst layer 32 surrounds the 22 and 23 where it acts as a support for the electrically-conductingchannels layer 25. Thedissipator 31 may be inserted in part in the thickness direction in a corresponding recess in thesupport 16, so that itsbottom surface 34 and a fraction of itsflanks 35 come into contact with the recess in thesupport 16, as shown inFigure 4 . - When electricity is caused to flow via the electrodes from an external source of a circuit for controlling operation of the initiator (not shown), heat is produced by the
heater resistor element 17. A fraction of this heat is diffused through thefirst layer 32 in theheat dissipator 31, passing from the dissipator through thesecond layer 33 into thesupport 16 or directly from theheat dissipator 31 into thesupport 16. Because of its structure and/or the material out of which it is made, i.e. in the embodiment shown in the figures, a polymer composite of the fiberglass-filled epoxy type, thesupport 16 dumps the heat coming from theheater resistor element 17. The presence of theheat dissipator 31 enables the value of the no-fire threshold to be set and raised so as to reduce the difference between the no-fire threshold and the all-fire threshold, as shown in the table below, where the no-fire current and the all-fire current are given with reliability of 99.9%, theelement 17 being made of NiCr, and where the no-fire current is raised by more than 44% by the presence of the dissipator. This makes the operation of the initiator more reliable.Initiator No-fire current in mA
(10 s/+90°C)All-fire current in mA
(2 ms/-40°C)With heat dissipator (17 micrometer thick copper layer) 551 1005 Without heat dissipator 381 998
Claims (9)
- An electropyrotechnic initiator comprising:- an ignition pyrotechnic charge (19, 21);- a heater resistor element (17) covered by the ignition pyrotechnic charge (19, 21);- two electrodes (12, 13) for feeding electricity to the heater resistor element (16); and- a support (16) for the heater resistor elements; andbetween the support (16) and the heater resistor element (17), and beneath at least the heater resistor element (17):- a heat dissipator (31) for dissipating heat produced by the heater resistor element (17) towards the support (16) ; the initiator being characterized in that it further comprises- a first layer (32) of heat-conducting and electrically-insulating adhesive interposed between the heater resistor element (17) and the heat dissipator (31).
- An electropyrotechnic initiator according to claim 1, characterized in that the heat dissipator (31) has a thermal conductivity greater than or equal to 100 mW/cm.K.
- An electropyrotechnic initiator according to claim 1 or 2, characterized in that a second layer (33) of heat-conducting and electrically-insulating adhesive is interposed between the heat dissipator (31) and the support (16).
- An electropyrotechnic initiator according to claim 1 or 2, characterized in that the heat dissipator (31) is in direct contact with the support (16).
- An electropyrotechnic initiator according to any preceding claim, characterized in that the heat dissipator (31) is formed by a heat-conducting layer (31).
- An electropyrotechnic initiator according to any preceding claim, characterized in that the heat dissipator (31) is made of a material selected from metal materials and ceramic materials.
- An electropyrotechnic initiator according to any preceding claim, characterized in that the heat dissipator (31) is made of a metal selected from copper, aluminum, alloys thereof, or oxides thereof.
- An electropyrotechnic initiator according to any preceding claim, characterized in that the heat dissipator (31) is located beneath the heater resistor element (17).
- An electropyrotechnic initiator according to any preceding claim, characterized in that the heater resistor element (17) is covered by two electrical contacts (26, 27) that are separate from each other and in contact with respective ones of the two electrodes (12, 13).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0401333A FR2866106B1 (en) | 2004-02-11 | 2004-02-11 | ELECTRO-PYROTECHNIC INITIATOR HAVING HEAT DISSIPATION |
| PCT/EP2005/001400 WO2005078377A1 (en) | 2004-02-11 | 2005-02-09 | An electropyrotechnic initiator with heat dissipation |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1716385A1 EP1716385A1 (en) | 2006-11-02 |
| EP1716385B1 true EP1716385B1 (en) | 2010-09-29 |
Family
ID=34778670
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP05707343A Expired - Lifetime EP1716385B1 (en) | 2004-02-11 | 2005-02-09 | An electropyrotechnic initiator with heat dissipation |
Country Status (6)
| Country | Link |
|---|---|
| EP (1) | EP1716385B1 (en) |
| JP (1) | JP4800975B2 (en) |
| AT (1) | ATE483149T1 (en) |
| DE (1) | DE602005023835D1 (en) |
| FR (1) | FR2866106B1 (en) |
| WO (1) | WO2005078377A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102014016923B3 (en) * | 2014-11-17 | 2016-02-25 | Elisabeth Dürschinger | Primer for occupant restraint systems |
| WO2016078634A1 (en) | 2014-11-17 | 2016-05-26 | Günter Dürschinger | Ignition capsule for occupant restraint systems |
| DE102015014124A1 (en) | 2015-11-03 | 2017-05-04 | Ems-Patvag s.r.o. | Primer for occupant restraint systems |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5774808B2 (en) | 2007-10-30 | 2015-09-09 | オートリブ ディベロップメント アクティエボラーグ | Electric ignition starter with heating resistance element |
| WO2010013930A2 (en) * | 2008-07-28 | 2010-02-04 | Lg Electronics Inc. | Reflector and gas oven range comprising the same |
| KR101578897B1 (en) | 2014-12-01 | 2015-12-17 | 주식회사 한화 | Low energy exploding foil assembly of primer detonator |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3227083A (en) * | 1964-01-30 | 1966-01-04 | Holex Inc | Electroexplosive cartridge with heat sink button |
| US3449999A (en) * | 1967-04-24 | 1969-06-17 | Myron A Coler | Method of making an electrical initiator |
| US3420174A (en) * | 1967-09-29 | 1969-01-07 | Us Navy | Pulse sensitive electro-explosive device |
| US3906858A (en) * | 1974-07-30 | 1975-09-23 | Us Eneregy Research And Dev Ad | Miniature igniter |
| US4103619A (en) * | 1976-11-08 | 1978-08-01 | Nasa | Electroexplosive device |
| JPH07324897A (en) * | 1994-05-30 | 1995-12-12 | Sensor Technol Kk | Ignition device |
| US5847309A (en) * | 1995-08-24 | 1998-12-08 | Auburn University | Radio frequency and electrostatic discharge insensitive electro-explosive devices having non-linear resistances |
-
2004
- 2004-02-11 FR FR0401333A patent/FR2866106B1/en not_active Expired - Fee Related
-
2005
- 2005-02-09 EP EP05707343A patent/EP1716385B1/en not_active Expired - Lifetime
- 2005-02-09 JP JP2006552560A patent/JP4800975B2/en not_active Expired - Fee Related
- 2005-02-09 DE DE602005023835T patent/DE602005023835D1/en not_active Expired - Lifetime
- 2005-02-09 AT AT05707343T patent/ATE483149T1/en not_active IP Right Cessation
- 2005-02-09 WO PCT/EP2005/001400 patent/WO2005078377A1/en not_active Ceased
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102014016923B3 (en) * | 2014-11-17 | 2016-02-25 | Elisabeth Dürschinger | Primer for occupant restraint systems |
| WO2016078634A1 (en) | 2014-11-17 | 2016-05-26 | Günter Dürschinger | Ignition capsule for occupant restraint systems |
| US10209041B2 (en) | 2014-11-17 | 2019-02-19 | Ems-Patvag s.r.o. | Detonator for passenger restraint systems |
| DE102015014124A1 (en) | 2015-11-03 | 2017-05-04 | Ems-Patvag s.r.o. | Primer for occupant restraint systems |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2866106A1 (en) | 2005-08-12 |
| JP2007522428A (en) | 2007-08-09 |
| EP1716385A1 (en) | 2006-11-02 |
| FR2866106B1 (en) | 2007-03-30 |
| WO2005078377A1 (en) | 2005-08-25 |
| ATE483149T1 (en) | 2010-10-15 |
| DE602005023835D1 (en) | 2010-11-11 |
| JP4800975B2 (en) | 2011-10-26 |
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