US20140245917A1 - Pyrotechnic time delay element - Google Patents
Pyrotechnic time delay element Download PDFInfo
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- US20140245917A1 US20140245917A1 US14/352,602 US201214352602A US2014245917A1 US 20140245917 A1 US20140245917 A1 US 20140245917A1 US 201214352602 A US201214352602 A US 201214352602A US 2014245917 A1 US2014245917 A1 US 2014245917A1
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- casing
- time delay
- delay element
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- Abandoned
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- 239000000203 mixture Substances 0.000 claims abstract description 30
- 239000012528 membrane Substances 0.000 claims abstract description 27
- 239000000463 material Substances 0.000 claims abstract description 25
- 239000002360 explosive Substances 0.000 claims abstract description 8
- 239000004033 plastic Substances 0.000 claims abstract description 8
- 229920003023 plastic Polymers 0.000 claims abstract description 8
- 230000015572 biosynthetic process Effects 0.000 claims description 5
- 238000005755 formation reaction Methods 0.000 claims description 5
- 229920001187 thermosetting polymer Polymers 0.000 claims description 4
- 229920001169 thermoplastic Polymers 0.000 claims description 3
- 239000004416 thermosoftening plastic Substances 0.000 claims description 3
- 230000000644 propagated effect Effects 0.000 claims description 2
- 230000005855 radiation Effects 0.000 claims description 2
- 239000007769 metal material Substances 0.000 claims 2
- 239000000835 fiber Substances 0.000 claims 1
- 238000000034 method Methods 0.000 description 6
- 238000001746 injection moulding Methods 0.000 description 5
- 239000004411 aluminium Substances 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 239000003365 glass fiber Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000003054 catalyst Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000007596 consolidation process Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C9/00—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
- F42C9/10—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by combustion
Definitions
- This invention relates to a time delay element for use in an explosive application.
- a time variation of the order of milliseconds can make a difference between a controlled blast with a good result and a complete blast failure with substantial cost implications.
- These time intervals can be controlled using electric or electronic systems and pyrotechnic delay systems.
- a typical chemical detonator system includes components such as a detonator shell which houses a high explosive base charge, a primary explosive charge and a time delay element.
- the delay element includes an aluminium casing that contains a pyrotechnic delay composition formed from a fuel/oxidiser mixture which, optionally, includes a metal powder or catalyst to control burning characteristics of the composition.
- the composition is press-loaded into the casing during a manufacturing step.
- the aluminium casing is normally manufactured by means of an extrusion process and is relatively expensive.
- the extrusion process results in a casing of a particular cross sectional shape and this poses a constraint on the shape of the composition which is loaded into the casing.
- Another factor is that recent detonator developments have been directed to metal-free systems and, from this point of view, the use of aluminium in making a detonator shell is not always desirable.
- An object of the present invention is to address, at least to some extent, the aforementioned factors.
- the invention provides a pyrotechnic time delay element which includes a casing which is formed from a suitable plastics material, the casing comprising a housing inside which is formed a volume, at least one opening to the volume and a pyrotechnic composition which is loaded into the volume through the opening.
- the pyrotechnic composition may be consolidated inside the volume after it has been loaded into the volume.
- the casing may be formed by means of a suitable moulding process e.g. an injection moulding process.
- the plastics material may be of any appropriate kind and may for example be a thermosetting or thermoplastics material which, optionally, is reinforced e.g. by the inclusion of fibres or which is otherwise treated e.g. by radiation, to enhance its mechanical properties.
- the plastics material may, itself, consist of a mixture of different injection mouldable materials and, optionally, fibres to enhance its properties so as to increase the strength of the material, to reduce the quantity of material required, or the like.
- the housing may be any suitable external cross sectional shape e.g. polygonal or circular, and may be tapered in longitudinal cross section and may have one or more internal or external step formations or the like.
- the housing may have a closed or sealed end which may be formed by the cap or which may be formed integrally with the remainder of the housing.
- the volume, in a longitudinal direction, may have a shape selected from the following: cylindrical, tapered, cylindrical with step formations, and a non-varying cross-sectional shape.
- a membrane may be positioned inside the volume separating an ignition end of the casing from the composition.
- the membrane may have a perforation or opening through it with a shape which, in cross-section, is selected from the following: circular, square, rectangular, cross shaped, star shaped, polygonal.
- the perforation or opening in the membrane, in a longitudinal direction of the casing, may vary in cross-sectional area.
- FIGS. 1 to 12 are side views in cross section of different casings for use in making a pyrotechnic time delay element, according to the invention.
- FIGS. 13 and 14 show, in cross section, different possible shapes of the casing
- FIGS. 15 to 18 show, in cross section, different membranes which can be used in a time delay element of the invention
- FIGS. 19 to 20 are side views of the membrane shown in FIGS. 15 to 18 respectively.
- FIGS. 23 to 27 are side views of other possible membranes which can be used in a time delay element according to the invention.
- the invention is concerned with a non-Metallic alternative to a typical metal time delay element casing.
- the casing of the invention is preferably made using injection moulding technology using a suitable plastic material or a mixture of plastic materials.
- the use of injection moulding techniques allows casings of various shapes to be made and also enables inner and outer surfaces of each casing to be varied according to requirement, within reason.
- thermoset or thermoplastic material When making the casing of the invention a suitable thermoset or thermoplastic material is selected. A requirement in this respect is that the chosen material should be capable of being injection moulded into an appropriate shape.
- Thermoset material if chosen, can be reinforced with carbon or glass fibre to achieve satisfactory strength characteristics. The material can also be treated after moulding to improve its mechanical properties.
- a thermoplastics material if chosen, can be reinforced with carbon or glass fibre to enhance its strength.
- FIG. 1 illustrates from one side and in longitudinal cross-section a typical casing 10 which is made in accordance with the principles of the invention.
- the casing is moulded from a suitable plastics material and has open opposed ends 12 and 14 respectively.
- the casing is filled with a suitable pyrotechnic composition 20 which is placed using any appropriate technique into an interior of the casing. Thereafter, the composition is press-loaded. Substantial force could be used to consolidate the composition in this way and it is essential therefore that the casing 10 must have sufficient strength not to deform during the consolidation process. Apart from this aspect it is to be borne in mind that when the composition is ignited it may then execute an extended timing interval of the order of seconds. The material which is used in the making of the casing must thus be adequately strong and have appropriate properties to enable the material to withstand the effects of the burning composition.
- FIG. 2 illustrates a casing 10 which has been press-loaded with a composition 20 , as described in connection with FIG. 1 , and wherein opposing ends 12 and 14 are sealed by means of respective closures or caps 22 which are forced into the open ends to achieve a tight sealed fit which ensures that the composition 20 is protected against extraneous factors.
- FIG. 3 shows the casing 10 , again filled with a composition in the manner described in connection with FIG. 1 , wherein a cap 28 is engaged over the open end 12 with an external surface of the casing. Similarly in FIG. 4 a second cap 30 is positioned over the opposing end 14 .
- the casing 12 shown in FIGS. 1 to 4 can be circular in cross section (transverse to a longitudinal axis) as is shown, for example, in FIG. 13 .
- the casing 10 has a polygonal shape.
- FIG. 14 depicts an octagonal shape—again this is exemplary only and non-limiting. If the shape is polygonal then this can be in the form of a regular or an irregular polygon, according to requirement.
- FIG. 5 shows a casing 40 which has a generally conical external shape 42 and a substantially similar generally conically tapered volume 46 which, in use, is loaded with a pyrotechnic composition.
- FIG. 6 shows a casing 48 which has an internal passage 50 of circular cylindrical configuration and an external shape 52 which is tapered. This construction results in one end 54 of the casing having a relatively thick side wall while an opposing end 56 has a thinner side wall.
- FIG. 7 shows a casing 60 of compound proportions.
- the casing includes three sections 62 , 64 and 66 respectively each of which has a respective internal volume 62 A, 64 A and 66 A respectively. These volumes differ in size from one another. Additionally, walls of the casing designated 62 B, 64 B and 66 B respectively, vary in thickness and hence in strength.
- FIG. 8 A different arrangement is embodied in a casing 70 shown in FIG. 8 .
- the casing has an internal volume 72 of circular cylindrical shape and of constant cross section from one end 74 to an opposing end 76 of the casing.
- a wall of the casing has a stepped configuration.
- An initial portion has a thickness 80
- an intermediate portion has a thickness 82 which is greater than the thickness 80
- a third section of the casing has a thickness 84 of maximum thickness.
- Geometrical variations of this kind i.e. variations in wall thickness, in the length of each wall and in the shape of each passage
- variations such as material types, reinforcements and so on, can all be employed, as appropriate, to obtain specific characteristics in the casing.
- FIG. 9 shows a casing 90 which has a regular circular outer shape 92 and an elongate tapered conical passage 94 .
- FIG. 10 shows a casing 96 which has a stepped internal configuration 98 with a regular circular cylindrical external shape 100 .
- FIG. 11 shows a casing 102 which has a tapered external shape 104 with a stepped internal configuration 106 .
- FIG. 12 illustrates an elongate casing 110 formed in an appropriate, injection-moulding process.
- the casing in this example, is in the form of a cylinder of circular cross section.
- a membrane 112 positioned inside a volume 114 , separates an ignition end 116 of the casing from a composition 118 which is placed inside the volume 114 .
- a primary explosive (not shown) is located preferably in the volume, on the ignition side of the membrane—this is the case for all the examples.
- the membrane may be solid or it may include at least one aperture or perforation of any appropriate shape or size.
- FIG. 15 for example illustrates a membrane 112 A which has a conical perforation 120 formed through it.
- FIG. 19 shows the perforation end-on.
- FIG. 16 shows a membrane 1126 with a circular perforation 122 and
- FIG. 20 shows the perforation end-on.
- FIG. 17 shows a membrane 112 C which has a perforation 124 which in cross section is tapered but which, viewed end-on as is shown in FIG. 21 , has a square cross section.
- FIG. 18 shows a membrane 112 D with a perforation 126 which, in cross section, is generally circular (see FIG. 22 ) although, viewed from one side, the perforation has a semi-spherical shape 128 .
- the membrane perforation varies in cross-sectional area.
- FIGS. 23 to 27 show different types of formations in various membranes.
- a membrane 130 has a mesh-like configuration.
- a membrane 132 has a slot 134 which is centrally positioned.
- a membrane 136 has a star-like section 138 while, in FIG. 26 , a membrane 140 is formed with a perforation or aperture 142 which is in the form of half of an annulus.
- a membrane 144 is formed with a cross-shaped perforation 146 .
- the various membranes and the cross sectional shapes of the perforation or perforations in the membranes can be used, as appropriate, to shape a wave-front which is propagated by the pyrotechnic composition to ensure that optimum ignition of a primary explosive takes place after the time delay element has executed its timing interval.
- a casing can be made in practically any form, shape or volume with the use of injection moulding techniques. Complex geometrical configurations are possible. These configurations can be used, as appropriate, to ensure that timing intervals are executed with a desired level of accuracy. Additionally, the casings do not make use of metallic sleeves.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
- Injection Moulding Of Plastics Or The Like (AREA)
Abstract
A pyrotechnic time delay element which includes a casing made from a plastics material, a pyrotechnic composition inside the volume, a membrane inside the volume against one end of the pyrotechnic composition and a primary explosive inside the volume on an opposing side of the membrane.
Description
- This invention relates to a time delay element for use in an explosive application.
- The ability to control the timing of an explosive detonator forms an integral part of blast design. A time variation of the order of milliseconds can make a difference between a controlled blast with a good result and a complete blast failure with substantial cost implications. These time intervals can be controlled using electric or electronic systems and pyrotechnic delay systems.
- A typical chemical detonator system includes components such as a detonator shell which houses a high explosive base charge, a primary explosive charge and a time delay element. Generally the delay element includes an aluminium casing that contains a pyrotechnic delay composition formed from a fuel/oxidiser mixture which, optionally, includes a metal powder or catalyst to control burning characteristics of the composition. Usually the composition is press-loaded into the casing during a manufacturing step.
- The aluminium casing is normally manufactured by means of an extrusion process and is relatively expensive. The extrusion process results in a casing of a particular cross sectional shape and this poses a constraint on the shape of the composition which is loaded into the casing. Another factor is that recent detonator developments have been directed to metal-free systems and, from this point of view, the use of aluminium in making a detonator shell is not always desirable.
- An object of the present invention is to address, at least to some extent, the aforementioned factors.
- The invention provides a pyrotechnic time delay element which includes a casing which is formed from a suitable plastics material, the casing comprising a housing inside which is formed a volume, at least one opening to the volume and a pyrotechnic composition which is loaded into the volume through the opening.
- The pyrotechnic composition may be consolidated inside the volume after it has been loaded into the volume.
- The casing may be formed by means of a suitable moulding process e.g. an injection moulding process.
- The plastics material may be of any appropriate kind and may for example be a thermosetting or thermoplastics material which, optionally, is reinforced e.g. by the inclusion of fibres or which is otherwise treated e.g. by radiation, to enhance its mechanical properties.
- The plastics material may, itself, consist of a mixture of different injection mouldable materials and, optionally, fibres to enhance its properties so as to increase the strength of the material, to reduce the quantity of material required, or the like.
- The housing may be any suitable external cross sectional shape e.g. polygonal or circular, and may be tapered in longitudinal cross section and may have one or more internal or external step formations or the like. The housing may have a closed or sealed end which may be formed by the cap or which may be formed integrally with the remainder of the housing.
- The volume, in a longitudinal direction, may have a shape selected from the following: cylindrical, tapered, cylindrical with step formations, and a non-varying cross-sectional shape.
- A membrane may be positioned inside the volume separating an ignition end of the casing from the composition. The membrane may have a perforation or opening through it with a shape which, in cross-section, is selected from the following: circular, square, rectangular, cross shaped, star shaped, polygonal.
- The perforation or opening in the membrane, in a longitudinal direction of the casing, may vary in cross-sectional area.
- The invention is further described by way of examples with reference to the accompanying drawings in which:
-
FIGS. 1 to 12 are side views in cross section of different casings for use in making a pyrotechnic time delay element, according to the invention, -
FIGS. 13 and 14 show, in cross section, different possible shapes of the casing, -
FIGS. 15 to 18 show, in cross section, different membranes which can be used in a time delay element of the invention, -
FIGS. 19 to 20 are side views of the membrane shown inFIGS. 15 to 18 respectively, and -
FIGS. 23 to 27 are side views of other possible membranes which can be used in a time delay element according to the invention. - The invention is concerned with a non-Metallic alternative to a typical metal time delay element casing. The casing of the invention is preferably made using injection moulding technology using a suitable plastic material or a mixture of plastic materials. The use of injection moulding techniques allows casings of various shapes to be made and also enables inner and outer surfaces of each casing to be varied according to requirement, within reason.
- When making the casing of the invention a suitable thermoset or thermoplastic material is selected. A requirement in this respect is that the chosen material should be capable of being injection moulded into an appropriate shape. Thermoset material, if chosen, can be reinforced with carbon or glass fibre to achieve satisfactory strength characteristics. The material can also be treated after moulding to improve its mechanical properties. Similarly, a thermoplastics material, if chosen, can be reinforced with carbon or glass fibre to enhance its strength.
- It is also possible to make a custom material by using a mixture of different injection mouldable materials and fillers, optionally with reinforcing, as may be appropriate.
-
FIG. 1 illustrates from one side and in longitudinal cross-section atypical casing 10 which is made in accordance with the principles of the invention. The casing is moulded from a suitable plastics material and has open 12 and 14 respectively.opposed ends - The casing is filled with a suitable
pyrotechnic composition 20 which is placed using any appropriate technique into an interior of the casing. Thereafter, the composition is press-loaded. Substantial force could be used to consolidate the composition in this way and it is essential therefore that thecasing 10 must have sufficient strength not to deform during the consolidation process. Apart from this aspect it is to be borne in mind that when the composition is ignited it may then execute an extended timing interval of the order of seconds. The material which is used in the making of the casing must thus be adequately strong and have appropriate properties to enable the material to withstand the effects of the burning composition. -
FIG. 2 illustrates acasing 10 which has been press-loaded with acomposition 20, as described in connection withFIG. 1 , and wherein 12 and 14 are sealed by means of respective closures oropposing ends caps 22 which are forced into the open ends to achieve a tight sealed fit which ensures that thecomposition 20 is protected against extraneous factors. -
FIG. 3 shows thecasing 10, again filled with a composition in the manner described in connection withFIG. 1 , wherein acap 28 is engaged over theopen end 12 with an external surface of the casing. Similarly inFIG. 4 asecond cap 30 is positioned over theopposing end 14. - The
casing 12 shown inFIGS. 1 to 4 can be circular in cross section (transverse to a longitudinal axis) as is shown, for example, inFIG. 13 . In a variation of the invention, shown inFIG. 14 (by way of example only), thecasing 10 has a polygonal shape.FIG. 14 depicts an octagonal shape—again this is exemplary only and non-limiting. If the shape is polygonal then this can be in the form of a regular or an irregular polygon, according to requirement. -
FIG. 5 shows acasing 40 which has a generally conicalexternal shape 42 and a substantially similar generally conically taperedvolume 46 which, in use, is loaded with a pyrotechnic composition.FIG. 6 shows acasing 48 which has aninternal passage 50 of circular cylindrical configuration and anexternal shape 52 which is tapered. This construction results in oneend 54 of the casing having a relatively thick side wall while anopposing end 56 has a thinner side wall. -
FIG. 7 shows acasing 60 of compound proportions. The casing includes three 62, 64 and 66 respectively each of which has a respectivesections 62A, 64A and 66A respectively. These volumes differ in size from one another. Additionally, walls of the casing designated 62B, 64B and 66B respectively, vary in thickness and hence in strength.internal volume - A different arrangement is embodied in a
casing 70 shown inFIG. 8 . The casing has aninternal volume 72 of circular cylindrical shape and of constant cross section from oneend 74 to anopposing end 76 of the casing. However a wall of the casing has a stepped configuration. An initial portion has athickness 80, an intermediate portion has a thickness 82 which is greater than thethickness 80, and a third section of the casing has athickness 84 of maximum thickness. Geometrical variations of this kind (i.e. variations in wall thickness, in the length of each wall and in the shape of each passage), and variations such as material types, reinforcements and so on, can all be employed, as appropriate, to obtain specific characteristics in the casing. -
FIG. 9 shows acasing 90 which has a regular circular outer shape 92 and an elongate taperedconical passage 94.FIG. 10 shows acasing 96 which has a steppedinternal configuration 98 with a regular circular cylindricalexternal shape 100.FIG. 11 shows acasing 102 which has a taperedexternal shape 104 with a steppedinternal configuration 106. -
FIG. 12 illustrates anelongate casing 110 formed in an appropriate, injection-moulding process. The casing, in this example, is in the form of a cylinder of circular cross section. Amembrane 112, positioned inside avolume 114, separates anignition end 116 of the casing from acomposition 118 which is placed inside thevolume 114. A primary explosive (not shown) is located preferably in the volume, on the ignition side of the membrane—this is the case for all the examples. - The membrane may be solid or it may include at least one aperture or perforation of any appropriate shape or size.
-
FIG. 15 for example illustrates amembrane 112A which has aconical perforation 120 formed through it.FIG. 19 shows the perforation end-on.FIG. 16 shows a membrane 1126 with acircular perforation 122 andFIG. 20 shows the perforation end-on.FIG. 17 shows amembrane 112C which has aperforation 124 which in cross section is tapered but which, viewed end-on as is shown inFIG. 21 , has a square cross section.FIG. 18 shows amembrane 112D with aperforation 126 which, in cross section, is generally circular (seeFIG. 22 ) although, viewed from one side, the perforation has asemi-spherical shape 128. Thus, in an axial direction of the casing, the membrane perforation varies in cross-sectional area. -
FIGS. 23 to 27 show different types of formations in various membranes. InFIG. 23 amembrane 130 has a mesh-like configuration. InFIG. 24 amembrane 132 has aslot 134 which is centrally positioned. InFIG. 25 amembrane 136 has a star-like section 138 while, inFIG. 26 , amembrane 140 is formed with a perforation oraperture 142 which is in the form of half of an annulus. InFIG. 27 on the other hand amembrane 144 is formed with across-shaped perforation 146. - The various membranes and the cross sectional shapes of the perforation or perforations in the membranes can be used, as appropriate, to shape a wave-front which is propagated by the pyrotechnic composition to ensure that optimum ignition of a primary explosive takes place after the time delay element has executed its timing interval.
- It is apparent from the aforegoing that a casing, according to the invention, can be made in practically any form, shape or volume with the use of injection moulding techniques. Complex geometrical configurations are possible. These configurations can be used, as appropriate, to ensure that timing intervals are executed with a desired level of accuracy. Additionally, the casings do not make use of metallic sleeves.
Claims (10)
1-11. (canceled)
12. A pyrotechnic time delay element which includes a casing which is injection-moulded from a non-metallic material, the casing comprising a housing inside which is formed a volume, at least one opening to the volume, a pyrotechnic composition which is loaded into the volume through the opening, and a membrane, inside the volume, which separates an ignition end of the casing from the composition, wherein the membrane has a perforation or opening with a shape, in cross-section, selected circular, square, rectangular, cross-shaped, star-shaped, polygonal, said membrane and cross sectional shape of perforation being used to shape a wave-front, propagated by the pyrotechnic composition, to ensure that optimum ignition of a primary explosive takes place after the time delay element has executed its timing interval.
13. A time delay element according to claim 12 wherein the pyrotechnic composition is consolidated inside the volume after it has been loaded into the volume.
14. A time delay element according to claim 12 wherein the non-metallic material is a plastics material selected from the following:
i. thermosetting material;
ii. thermoplastics material;
iii. material which is reinforced by the inclusion of fibers or by means of radiation;
iv. mixture of injection-mouldable materials.
15. A time delay element according to claim 12 wherein the housing has an external cross-sectional shape selected from the following: circular and polygonal; and, in a longitudinal direction, has a shape selected from the following:
cylindrical; tapered; and cylindrical with step formations.
16. A time delay element according to claim 12 wherein opposed ends of the housing are sealed by means of respective closures to protect the pyrotechnic composition which is inside the volume.
17. A time delay element according to claim 12 wherein the casing has a wall, around the volume, of constant thickness.
18. A time delay element according to claim 12 wherein the casing has a wall, around the volume, of varying thickness.
19. A time delay element according to claim 12 wherein the perforation or opening in the membrane, in a longitudinal direction of the casing, varies in cross-sectional area.
20. A time delay element according to claim 12 wherein the volume, in a longitudinal direction, has a shape selected from the following: cylindrical, tapered, cylindrical with step formations, and a non-varying cross-sectional shape.
Applications Claiming Priority (3)
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|---|---|---|---|
| ZA2011/07996 | 2011-10-17 | ||
| ZA201107996 | 2011-10-17 | ||
| PCT/ZA2012/000070 WO2013059841A1 (en) | 2011-10-17 | 2012-10-16 | Pyrotechnic time delay element |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20140245917A1 true US20140245917A1 (en) | 2014-09-04 |
Family
ID=47192241
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US14/352,602 Abandoned US20140245917A1 (en) | 2011-10-17 | 2012-10-16 | Pyrotechnic time delay element |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US20140245917A1 (en) |
| EP (1) | EP2769170B1 (en) |
| AP (1) | AP2014007504A0 (en) |
| AU (1) | AU2012325733A1 (en) |
| CA (1) | CA2848612A1 (en) |
| CL (1) | CL2014000951A1 (en) |
| ES (1) | ES2559362T3 (en) |
| PE (1) | PE20142086A1 (en) |
| PL (1) | PL2769170T3 (en) |
| WO (1) | WO2013059841A1 (en) |
| ZA (1) | ZA201401724B (en) |
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| US2436305A (en) * | 1944-02-03 | 1948-02-17 | Remington Arms Co Inc | Ammunition |
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| US4742773A (en) * | 1986-10-03 | 1988-05-10 | The Ensign-Bickford Company | Blasting signal transmission tube delay unit |
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| USH866H (en) * | 1986-07-17 | 1991-01-01 | The United States Of America As Represented By The Secretary Of The Navy | Shaped charge assembly |
| US5031538A (en) * | 1990-02-07 | 1991-07-16 | The Ensign-Bickford Company | Delay train ignition buffer |
| US5522318A (en) * | 1990-11-05 | 1996-06-04 | The Ensign-Bickford Company | Cushion element for detonators and the like; apparatus and method of assembly |
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| US6470806B1 (en) * | 2000-02-28 | 2002-10-29 | Kenneth R. Murray | Cartridge format delay igniter |
| US6640719B1 (en) * | 1999-01-11 | 2003-11-04 | The United States Of America As Represented By The Secretary Of The Army | Fuze explosive train device and method |
| US20040060625A1 (en) * | 2002-10-01 | 2004-04-01 | The Regents Of The University Of California. | Nano-laminate-based ignitors |
| US20070101889A1 (en) * | 2003-04-30 | 2007-05-10 | James Bayliss | Tubular signal transmission device and method of manufacture |
| US20100064924A1 (en) * | 2005-02-08 | 2010-03-18 | John Childs | Delay units and methods of making the same |
| US7792495B2 (en) * | 2004-11-15 | 2010-09-07 | Kyocera Corporation | Radio apparatus, transmission control method and transmission control program |
| US7992495B2 (en) * | 2006-03-24 | 2011-08-09 | African Explosives Limited | Detonation of explosives |
| US8037827B2 (en) * | 2008-07-11 | 2011-10-18 | Junghans Microtec Gmbh | Fuze for a projectile |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AU2007215065A1 (en) * | 2006-02-13 | 2007-08-23 | Dyno Nobel Inc. | Delay elements, detonators containing the same and methods of making |
| AP2640A (en) * | 2006-03-24 | 2013-04-11 | Ael Mining Services Ltd | Detonation of explosives |
-
2012
- 2012-10-16 US US14/352,602 patent/US20140245917A1/en not_active Abandoned
- 2012-10-16 AP AP2014007504A patent/AP2014007504A0/en unknown
- 2012-10-16 ES ES12788097.9T patent/ES2559362T3/en active Active
- 2012-10-16 PE PE2014000551A patent/PE20142086A1/en not_active Application Discontinuation
- 2012-10-16 PL PL12788097T patent/PL2769170T3/en unknown
- 2012-10-16 AU AU2012325733A patent/AU2012325733A1/en not_active Abandoned
- 2012-10-16 CA CA2848612A patent/CA2848612A1/en not_active Abandoned
- 2012-10-16 WO PCT/ZA2012/000070 patent/WO2013059841A1/en not_active Ceased
- 2012-10-16 EP EP12788097.9A patent/EP2769170B1/en not_active Not-in-force
-
2014
- 2014-03-10 ZA ZA2014/01724A patent/ZA201401724B/en unknown
- 2014-04-14 CL CL2014000951A patent/CL2014000951A1/en unknown
Patent Citations (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2436305A (en) * | 1944-02-03 | 1948-02-17 | Remington Arms Co Inc | Ammunition |
| US2944486A (en) * | 1954-01-21 | 1960-07-12 | Hotchkiss Brandt | Self-propelled projectile |
| US4753170A (en) * | 1983-06-23 | 1988-06-28 | Jet Research Center | Polygonal detonating cord and method of charge initiation |
| USH866H (en) * | 1986-07-17 | 1991-01-01 | The United States Of America As Represented By The Secretary Of The Navy | Shaped charge assembly |
| US4742773A (en) * | 1986-10-03 | 1988-05-10 | The Ensign-Bickford Company | Blasting signal transmission tube delay unit |
| US5031538A (en) * | 1990-02-07 | 1991-07-16 | The Ensign-Bickford Company | Delay train ignition buffer |
| US5522318A (en) * | 1990-11-05 | 1996-06-04 | The Ensign-Bickford Company | Cushion element for detonators and the like; apparatus and method of assembly |
| US6062143A (en) * | 1997-09-08 | 2000-05-16 | Simula, Inc. | Distributed charge inflator system |
| US6640719B1 (en) * | 1999-01-11 | 2003-11-04 | The United States Of America As Represented By The Secretary Of The Army | Fuze explosive train device and method |
| US6470806B1 (en) * | 2000-02-28 | 2002-10-29 | Kenneth R. Murray | Cartridge format delay igniter |
| US20040060625A1 (en) * | 2002-10-01 | 2004-04-01 | The Regents Of The University Of California. | Nano-laminate-based ignitors |
| US20070101889A1 (en) * | 2003-04-30 | 2007-05-10 | James Bayliss | Tubular signal transmission device and method of manufacture |
| US7792495B2 (en) * | 2004-11-15 | 2010-09-07 | Kyocera Corporation | Radio apparatus, transmission control method and transmission control program |
| US20100064924A1 (en) * | 2005-02-08 | 2010-03-18 | John Childs | Delay units and methods of making the same |
| US7992495B2 (en) * | 2006-03-24 | 2011-08-09 | African Explosives Limited | Detonation of explosives |
| US8037827B2 (en) * | 2008-07-11 | 2011-10-18 | Junghans Microtec Gmbh | Fuze for a projectile |
Also Published As
| Publication number | Publication date |
|---|---|
| CL2014000951A1 (en) | 2014-08-08 |
| WO2013059841A1 (en) | 2013-04-25 |
| PL2769170T3 (en) | 2016-06-30 |
| ZA201401724B (en) | 2014-12-23 |
| AU2012325733A1 (en) | 2014-04-03 |
| EP2769170A1 (en) | 2014-08-27 |
| CA2848612A1 (en) | 2013-04-25 |
| ES2559362T3 (en) | 2016-02-11 |
| EP2769170B1 (en) | 2015-12-16 |
| PE20142086A1 (en) | 2014-12-06 |
| AP2014007504A0 (en) | 2014-03-31 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: AEL MINING SERVICES LIMITED, SOUTH AFRICA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:BEZUIDENHOUT, HENDRIK CORNELIUS;HALLIDAY, PIETER STEPHANUS JACOBUS;REEL/FRAME:032775/0509 Effective date: 20140417 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |