GB2224729A - Pyrotechnic train - Google Patents
Pyrotechnic train Download PDFInfo
- Publication number
- GB2224729A GB2224729A GB8919489A GB8919489A GB2224729A GB 2224729 A GB2224729 A GB 2224729A GB 8919489 A GB8919489 A GB 8919489A GB 8919489 A GB8919489 A GB 8919489A GB 2224729 A GB2224729 A GB 2224729A
- Authority
- GB
- United Kingdom
- Prior art keywords
- films
- train
- pyrotechnic train
- pyrotechnic
- substrate
- 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.)
- Granted
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
- C06B45/12—Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones
- C06B45/14—Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones a layer or zone containing an inorganic explosive or an inorganic explosive or an inorganic thermic component
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
- C06C5/00—Fuses, e.g. fuse cords
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
-
- 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
- F42B3/16—Pyrotechnic delay initiators
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- General Engineering & Computer Science (AREA)
- Inorganic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Air Bags (AREA)
Abstract
A pyrotechnic train is formed from a reactive laminate of thin films of an electron acceptor material 9, e.g. lead oxide, and an electron donor material e.g. titanium, 10, alternately vapour deposited upon a substrate 1. Selective etching or selective masking techniques are used to leave a desired network of reaction progression paths 2 for a sealed delay train or track plate for ignition. The thickness of the films is of substantially molecular order to maximise molecular intermingling between them. Ignition of the conjoint films at any selected location initiates a self-sustaining exothermic reaction which progresses laterally along the film interfaces, and may be modulated by one or more layers 11, e.g. silicon. The reactive laminate is also applicable as a heat radiation emitter, and as a bridge igniter for a detonator in place of a conventional exploding bridge wire between electrodes. <IMAGE>
Description
Pyrotechnic Train
This invention relates to a pyrotechnic train, in particular but not exclusively, suitable for use in single or multitrain delay systems. It is also applicable to bridgewire detonators and may be further adapted to provide infra-red radiation emitting coatings for decoy systems.
Multi-train pyrotechnic delay systems are known for initiating complex sequences of events, in a missile for example.
These delay systems are normally constucted from known delay cords comprising lead tubes which are first packed with a prepared granular pyrotechnic composition, consisting of materials which are selected, prepared and mixed in specific ratios to achieve desired burning rates. The packed tubes are then fine drawn, cut to length, shaped and manually assembled with appropriate coupling components.
The whole process is lengthy and operator dependent, has high tooling costs, requires clean room assembly and can be hazardous.
The resulting multi-train is also disadvantageous in having a number of undesirable interfaces and inconsistent burning times.
Furthermore there are problems attendant upon the use of such multitrain systems within an enclosed capsule in that the lead casing, which melts during burning, becomes spattered around possibly damaging other items in the capsule, such as plastics materials casings. Also, the pressure of the gases generated during burning by the fairly large volume of pyrotechnic composition can be embarassingly high especially when the capsule is used at very low ambient pressure.
The present invention seeks to overcome these difficulties by providing a pyrotechnic train capable of having greater precision and greater inherent strength than that achievable with granular compositions, and having a production method amenable to automation.
Further, in a first aspect of the invention, the invention seeks to provide a fully sealable delay train.
In a second aspect, the invention seeks to provide an exposable pyrotechnic train which, when ignited, will radiate a pre-determined spectrum of wavelengths, and in a third aspect the invention seeks to provide a bridge ignitor having a reaction time comparable with that of an exploding bridgewire, but having greater reliability.
In accordance with the present invention, a pyrotechnic train includes a reactive laminate comprised by a plurality of films of an electron donor material alternately interlayered with a plurality of films of an electron acceptor material, each sequentially vapour deposited upon a substrate, the said two materials being conjointly capable of exothermic reaction when subjected to heat.
Preferably, each film is subsequentially deposited by vacuum deposition or by sputtering, the deposition process being controlled to ensure that the thickness of each film is of substantially molecular order so as to maximise molecular intermingling of the film materials throughout the thickness of the laminate.
Ignition of the conjoint electron donor and electron acceptor films at any selected location initiates a selfsustaining, exothermic reaction between the molecules which progresses laterally along the film interfaces. The number and thickness of the films is selected to be sufficient to ensure a reliable and consistent lateral progression characteristic.
The reactive laminate may further include one or more films of a moderating material selectively interlayered with the said reactive films during the deposition process so as to moderate the lateral progression characteristic, thereby to achieve a desired burning rate. The moderating material may also be selected to inject desired frequencies into the resulting radiation spectrum.
In the first aspect of the invention, ie a sealable delay train, the substrate comprises an inert material which is preferably a poor thermal conductor so as to minimise diminution of the exothermic reaction, and may conveniently be a glass or ceramic material. If however, further moderation or variation of the progression characteristic is desired the thermal conductivity of the support member may be appropriately selected.
The lateral dimensions of the reactive laminate are selected to define the width and length of a desired reaction progression path. These may be determined by the configuration of the substrate itself. The films may be deposited upon one whole surface of a planar substrate and subsequently processed by known printed circuit techniques, to produce any desired planar configuration of progression path. In an alternative method, the planar substrate may be masked prior to deposition so as to permit deposition of the reactive films upon the substrate in the desired configuration only.
Either of these latter two planar methods is particularly advantageous for the manufacture of complex multi-train systems, as the integral deposition of all the progression paths of the system thus made possible eliminates the need for undesirable interconnections.
A planar arrangement is also to be preferred in the first aspect of the invention when sealed confinement of the progression paths is required, an overlaid cover of ptfe or of an inert material, preferably of low thermal conductivity, being readily sealable to the substrate. Such confinement acts both to contain the reaction and to control the pressure of the reaction and hence the burning rate. Consequently the closeness of confinement may be varied to provide further control of the progression characteristic.
In a second aspect of the invention, ie a radiation emitter, reactive and moderating materials are selectively employed to provide a heat output train having a specific radiation spectrum.
In the third aspect of the invention, ie a bridge ignitor, the reactive laminate is used to provide a brisant reaction progression path between two electrodes adjacent a detonating charge, the laminate being vapour-deposited directly upon a conventional insulating support for the electrodes.
Embodiments of the invention and methods of manufacture will now be described by way of example only, with reference to the accompanying drawings of which
Figure 1 is a plan view of a sealed planar pyrotechnic multi-train,
Figure 2 is a sectioned elevation taken on the line II-II of Figure 1,
Figure 3 is a sectioned elevation of an alternative terminal arrangement for the multi-train of Figure 1, and
Figure 4 is an axially sectioned view of a bridge ignitor.
The pyrotechnic multi-train illustrated in Figures 1 and 2 comprises a ceramic support plate 1 upon which is superimposed a network of reactive laminate progression paths 2 variously interconnecting and extending into edge terminals 3 to 7. The network of paths 2 is overlaid by a correspondingly configured cover 8 of ceramic which is peripherally sealed to the support plate 1, except at the terminals 3 to 7.
Each path 2 comprises a stack of alternately deposited coreactive films 9 and 10, and has one interleaved moderating film 11.
The films 9 and 10 are respectively of electron acceptor and electron donor materials, those used in the present example being lead oxide for films 9 and titanium for films 10. Film 11 is optional and may be of an inert material such as silicon.
The paths 2 are formed upon the plate 1 in a method of manufacture now to be described.
One whole face of the support plate 1 is first suitably prepared and then completely coated with the films 9, 10 and 11 in appropriate sequence using conventional vacuum deposition equipment (not shown). The deposition source materials, eg lead oxide, titanium and silicon, are each located in separate vaporising boats and vaporised in turn by electron beam in an atmosphere of argon.
To ensure a reliable reaction progression characteristic the thickness of each deposited film 9, 10 and 11 is preferably no greater than 2ftm, films of greater thickness being undesirable as their heat of absorption may be sufficient to destroy the exothermic nature of the interlayer reaction. The total number of reaction films 9 and 10 required is dependent upon the thickness and the thermal conductivity of the support plate, ie upon its effectiveness as a heat sink. Using an
uluminow aluminiu support plate of lmm thickness having a thermal conductivity of 17W/m, a deposition of 100 films 9 and 100 films 10, each of 0.5 m thickness, has been found effective. (Only a few films are illustrated in the interest of clarity).
The thus deposited films 9, 10 and 11 each have a columnar crystal lattice structure which is intermolecularly engaged with each next adjacent lattice providing a reactive laminate which once ignited will sustain an inter-lattice exothermic reaction.
After completion of the deposition process, the required areas of the deposited laminate, ie the network of paths 2, are masked with an acid resistant coating (not shown) and the remaining areas of the films removed by acid etching in the manner of known printed circuit board production techniques. The plate 8 is then superimposed and edge-sealed to the support plate 1, by means of a compatible sealant (not shown).
It will be apparent to those skilled in the art that a similar network of paths 2 can be alternatively achieved by masking the support plate prior to deposition of the film 9, 10 and 11.
In use, the progression path network is ignited electrically, or by friction or by heat donor source at a selected one of the terminals, terminal 3 for example, and the resulting exothermic reaction progresses along the paths 2 at uniform rate to provide an ignition source at each of the remaining terminals 4 to 7 at intervals precisely determined by the lengths of the intervening paths. In application, all or any of the terminals 4 to 7 may be used to initiate other ongoing delays or terminal events.
A further alternative method of manufacture requires the use of a photo sensitive glass for the support plate 1, of a type well known for printed circuit production, which is rendered less resistant to exposure to ultra-violet radiation. The plate 1 of this material can be first masked with the desired configuration of progression paths, exposed to ultra-violet radiation, and then etched so as to form a pierced template of the path network, which template is subsequently subjected to vacuum deposition of the reactive laminate as previously described. Sealing of the progression paths manufactured in this manner may be achieved by encapsulating the coated template between the cover 8 and a supplementary base plate (not shown).
An alternative terminal arrangement is illustrated in
Figure 3 for use when access to the multi-train is required through the thickness of the plate 1. In this arrangement, suitably shaped holes 12 are provided in the plate 1 before the commencement of the deposition process, the edges of which holes become coated with the reactive laminate during subsequent deposition in common with the planar surface of the plate.
It will be apparent to those skilled in the art that other, more complex delay train networks can be produced in accordance with the invention. For example, specialised event initiators can be formed integrally with the paths at selected terminals during manufacture. In addition, alternative routes can be built into any particular multi-train so as to permit selection of delay times.
The first aspect of the invention is also applicable to the manufacture of track plates for the provision of multiple simultaneous ignition for the initiation of explosive or pyrotechnic devices in a wide variety of geometric configurations.
The vapour deposited reactive laminate of the invention is inherently stronger than granular- pyrotechnic compositions and is therefore advantageous in use in the second aspect of the invention, in that no protective external covering is required. In this aspect the reactive and moderating materials employed in the laminate can be selected to provide a heat output train having a specific radiation spectrum. A further advantage lies in the wide choice of materials that can be readily vapour deposited thus permitting provision of a comprehensive range of wavelengths in the radiation spectrum.
In its third aspect, the invention provides a ready means of fabricating electrically sensitive detonators and igniferous initiators. A conventional cylindrical arrangement is illustrated in Figure 4, in which a first electrode in the form of a pin 40 is held coaxially within a cylindrical second electrode 41 by means of an insulating bush 42, the reactive laminate 43 being deposited directly onto the annular end face of the bush adjacent a detonator charge 44, thereby providing a reliable multi-radial reaction progression path between the two electrodes capable of violent reaction at relatively low voltage. Such arrangements can also be used as an ignitor, merely by reducing the voltage applied to the electrodes.
Another similar application of the invention is in the preparation of fast acting electrical cut-out fuses (not shown).
Claims (9)
1. A pyrotechnic train including a reactive laminate comprised by a plurality of films of an electron donor material alternately interlayered with a plurality of films of an electron acceptor material, each sequentially vapour deposited upon a substrate, the said two materials being conjointly capable of exothermic reaction when subjected to heat.
2. A pyrotechnic train as claimed in claim 1 further including at least one interlayered film of a moderating material.
3. A pyrotechnic train as claimed in claim 1 or claim 2 wherein the thickness of each film is not greater than 2 microns.
4. A pyrotechnic train as claimed in any one of claims 1 to 3 wherein the electron acceptor material is lead oxide and the electron donor material is titanium.
5. A pyrotechnic train as claimed in any one of the preceding claims arranged as a bridge between two electrodes located adjacent a detonator charge.
6. A method of manufacture for a pyrotechnic train as claimed in any one of claims 1 to 4 wherein a desired configuration of reaction progression paths is provided by the removal of unwanted regions of the deposited plurality of films from the substrate by a process of selective etching.
7. A method of manufacture for a pyrotechnic train as claimed in any one of claims 1 to 4 wherein the substrate is selectively masked prior to deposition so as to deposit the plurality of films in a desired configuration of reaction progression paths.
8. A pyrotechnic train substantially as hereinbefore described with reference to the accompanying Figures 1 to 3.
9. A method of manufacture for a pyrotechnic train substantially as hereinbefore described with reference to the accompanying Figures 1 to 3.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8615457 | 1986-06-25 | ||
GB878712789A GB8712789D0 (en) | 1986-06-25 | 1987-06-01 | Pyrotechnic train |
FI894051A FI100469B (en) | 1986-06-25 | 1989-08-29 | Pyrotechnic ignition cable |
IL9149789A IL91497A (en) | 1986-06-25 | 1989-09-01 | Pyrotechnic train |
BR898904455A BR8904455A (en) | 1986-06-25 | 1989-09-04 | PIROTECHNICAL TRAIN AND MANUFACTURING PROCESS |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8919489D0 GB8919489D0 (en) | 1989-10-18 |
GB2224729A true GB2224729A (en) | 1990-05-16 |
GB2224729B GB2224729B (en) | 1990-07-25 |
Family
ID=27507818
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8919489A Expired - Lifetime GB2224729B (en) | 1986-06-25 | 1989-08-29 | Pyrotechnic train |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2224729B (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2260317A (en) * | 1991-10-08 | 1993-04-14 | Us Energy | Energetic composites and method of providing chemical energy |
GB2266944A (en) * | 1992-05-12 | 1993-11-17 | Marconi Gec Ltd | Flare arrangements |
WO1994024074A1 (en) * | 1993-04-15 | 1994-10-27 | The Secretary Of State For Defence | Pyrotechnic material |
GB2291642A (en) * | 1993-04-15 | 1996-01-31 | Secr Defence | Pyrotechnic material |
DE10015070A1 (en) * | 2000-03-25 | 2001-10-11 | Daimler Chrysler Ag | Explosive charge for a warhead |
WO2002079713A1 (en) * | 2001-03-31 | 2002-10-10 | Robert Bosch Gmbh | Bridge igniter |
DE10125226A1 (en) * | 2001-05-23 | 2002-12-05 | Tdw Ges Fuer Wehrtechnische Wi | Warhead comprises intermediate layer comprising separating layers and explosive filling in intermediate chamber between separating layers |
WO2009017880A2 (en) * | 2007-08-02 | 2009-02-05 | Ensign-Bickford Aerospace & Defense Company | Slow burning, gasless heating elements |
US7748323B2 (en) | 2004-10-04 | 2010-07-06 | Nipponkayaku Kabushikikaisha | Semiconductor bridge device and igniter including semiconductor bridge circuit device |
WO2013016116A1 (en) * | 2011-07-22 | 2013-01-31 | Nanocomposix, Inc. | Pyrophoric sheet |
US8608878B2 (en) | 2010-09-08 | 2013-12-17 | Ensign-Bickford Aerospace & Defense Company | Slow burning heat generating structure |
RU177296U1 (en) * | 2017-09-18 | 2018-02-15 | Российская Федерация, от имени которой выступает Федеральное государственное казенное учреждение "Войсковая часть 68240" | MULTILAYER STRUCTURES IGNITION |
RU2798415C1 (en) * | 2022-07-26 | 2023-06-22 | Акционерное общество "Омский научно-исследовательский институт приборостроения" (АО "ОНИИП") | Pyrotechnic energy igniter |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4080902A (en) * | 1976-11-04 | 1978-03-28 | Teledyne Mccormick Selph | High speed igniter device |
GB2190730A (en) * | 1986-05-22 | 1987-11-25 | Detonix Close Corp | Detonator firing element |
-
1989
- 1989-08-29 GB GB8919489A patent/GB2224729B/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4080902A (en) * | 1976-11-04 | 1978-03-28 | Teledyne Mccormick Selph | High speed igniter device |
GB2190730A (en) * | 1986-05-22 | 1987-11-25 | Detonix Close Corp | Detonator firing element |
Cited By (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2260317A (en) * | 1991-10-08 | 1993-04-14 | Us Energy | Energetic composites and method of providing chemical energy |
GB2260317B (en) * | 1991-10-08 | 1995-11-08 | Us Energy | Energetic composites and method of providing chemical energy |
GB2266944A (en) * | 1992-05-12 | 1993-11-17 | Marconi Gec Ltd | Flare arrangements |
GB2266944B (en) * | 1992-05-12 | 1995-08-02 | Marconi Gec Ltd | Flare arrangements |
WO1994024074A1 (en) * | 1993-04-15 | 1994-10-27 | The Secretary Of State For Defence | Pyrotechnic material |
GB2291642A (en) * | 1993-04-15 | 1996-01-31 | Secr Defence | Pyrotechnic material |
GB2291642B (en) * | 1993-04-15 | 1997-06-04 | Secr Defence | Pyrotechnic material |
DE10015070B4 (en) * | 2000-03-25 | 2005-05-04 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Explosive charge for a warhead |
DE10015070A1 (en) * | 2000-03-25 | 2001-10-11 | Daimler Chrysler Ag | Explosive charge for a warhead |
US6810815B2 (en) | 2001-03-31 | 2004-11-02 | Robert Bosch Gmbh | Bridge igniter |
WO2002079713A1 (en) * | 2001-03-31 | 2002-10-10 | Robert Bosch Gmbh | Bridge igniter |
DE10125226A1 (en) * | 2001-05-23 | 2002-12-05 | Tdw Ges Fuer Wehrtechnische Wi | Warhead comprises intermediate layer comprising separating layers and explosive filling in intermediate chamber between separating layers |
DE10125226C2 (en) * | 2001-05-23 | 2003-11-27 | Tdw Verteidigungstech Wirksys | Explosive charge for a warhead |
US7748323B2 (en) | 2004-10-04 | 2010-07-06 | Nipponkayaku Kabushikikaisha | Semiconductor bridge device and igniter including semiconductor bridge circuit device |
US7930976B2 (en) | 2007-08-02 | 2011-04-26 | Ensign-Bickford Aerospace & Defense Company | Slow burning, gasless heating elements |
WO2009017880A3 (en) * | 2007-08-02 | 2009-09-24 | Ensign-Bickford Aerospace & Defense Company | Slow burning, gasless heating elements |
WO2009017880A2 (en) * | 2007-08-02 | 2009-02-05 | Ensign-Bickford Aerospace & Defense Company | Slow burning, gasless heating elements |
US8608878B2 (en) | 2010-09-08 | 2013-12-17 | Ensign-Bickford Aerospace & Defense Company | Slow burning heat generating structure |
WO2013016116A1 (en) * | 2011-07-22 | 2013-01-31 | Nanocomposix, Inc. | Pyrophoric sheet |
GB2507232A (en) * | 2011-07-22 | 2014-04-23 | Nanocomposix Inc | Pyrophoric sheet |
US8852731B2 (en) | 2011-07-22 | 2014-10-07 | Nanocomposix, Inc. | Pyrophoric sheet |
GB2507232B (en) * | 2011-07-22 | 2015-05-06 | Nanocomposix Inc | Pyrophoric sheet |
RU177296U1 (en) * | 2017-09-18 | 2018-02-15 | Российская Федерация, от имени которой выступает Федеральное государственное казенное учреждение "Войсковая часть 68240" | MULTILAYER STRUCTURES IGNITION |
RU2798415C1 (en) * | 2022-07-26 | 2023-06-22 | Акционерное общество "Омский научно-исследовательский институт приборостроения" (АО "ОНИИП") | Pyrotechnic energy igniter |
Also Published As
Publication number | Publication date |
---|---|
GB8919489D0 (en) | 1989-10-18 |
GB2224729B (en) | 1990-07-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5090322A (en) | Pyrotechnic train | |
US4976200A (en) | Tungsten bridge for the low energy ignition of explosive and energetic materials | |
KR0167081B1 (en) | Pyrotechnic materials | |
GB2224729A (en) | Pyrotechnic train | |
EP0279796B1 (en) | Detonator | |
US4788913A (en) | Flying-plate detonator using a high-density high explosive | |
EP0147696B1 (en) | Miniaturized monolithic multi-layer capacitor and apparatus and method for making | |
US20070056459A1 (en) | Titanium semiconductor bridge igniter | |
US6133146A (en) | Semiconductor bridge device and method of making the same | |
DE2104273A1 (en) | Process for the explosive connection of workpieces | |
US5682008A (en) | Monolithic semiconductor igniter for explosives and pyrotechnic mixtures and a process for manufacturing therefore | |
RU2120930C1 (en) | Pyrotechnic material and method of its manufacture | |
CN109425266B (en) | Based on Al/MxOyInterdigital structure energy-exchanging element containing energy film | |
US3457726A (en) | Incrementally controllable-thrust propulsion device | |
NL193758C (en) | Pyrotechnic chain. | |
GB2033553A (en) | Electric priming devices | |
US4174944A (en) | Single lead electrically-activated flashlamp | |
AU2011224469A1 (en) | Sealer elements, detonators containing the same, and methods of making | |
FR2538207B1 (en) | PROCESS FOR THE MANUFACTURE OF AN ELECTRIC CIRCUIT FOR THE FIRE OF A PYROTECHNIC DEVICE AND CIRCUIT THUS OBTAINED | |
NO171751B (en) | PYROTECHNICAL CHAIN AND PROCEDURES FOR ITS MANUFACTURING | |
US4101953A (en) | Multiple flashlamp array | |
US4432723A (en) | Multilamp photoflash unit with improved quick-disconnect switch | |
US4311453A (en) | High voltage flashlamp with ignition means including a plurality of spark gap members | |
US8020490B1 (en) | Method of fabricating MEMS-based micro detonators | |
EP0029523B1 (en) | Miniature photoflash lamp and method of making |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
732E | Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |