US3610151A - Nonelectric squib assembly - Google Patents
Nonelectric squib assembly Download PDFInfo
- Publication number
- US3610151A US3610151A US823351A US3610151DA US3610151A US 3610151 A US3610151 A US 3610151A US 823351 A US823351 A US 823351A US 3610151D A US3610151D A US 3610151DA US 3610151 A US3610151 A US 3610151A
- Authority
- US
- United States
- Prior art keywords
- squib
- chamber
- firing pin
- motor
- assembly
- 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
Links
- 238000010304 firing Methods 0.000 claims abstract description 25
- 239000007789 gas Substances 0.000 claims abstract description 15
- 238000009527 percussion Methods 0.000 claims abstract description 6
- 239000002131 composite material Substances 0.000 claims description 5
- 229910001209 Low-carbon steel Inorganic materials 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 239000011888 foil Substances 0.000 claims description 3
- 239000010445 mica Substances 0.000 claims description 3
- 229910052618 mica group Inorganic materials 0.000 claims description 3
- 238000007789 sealing Methods 0.000 claims description 2
- 238000000926 separation method Methods 0.000 claims description 2
- OLRXHZHVFRYMHO-UHFFFAOYSA-N [N+](=O)([O-])[O-].[K+].[B+3].[N+](=O)([O-])[O-].[N+](=O)([O-])[O-].[N+](=O)([O-])[O-] Chemical compound [N+](=O)([O-])[O-].[K+].[B+3].[N+](=O)([O-])[O-].[N+](=O)([O-])[O-].[N+](=O)([O-])[O-] OLRXHZHVFRYMHO-UHFFFAOYSA-N 0.000 abstract description 3
- 238000010008 shearing Methods 0.000 description 2
- 235000003197 Byrsonima crassifolia Nutrition 0.000 description 1
- 240000001546 Byrsonima crassifolia Species 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 101150090410 NEFL gene Proteins 0.000 description 1
- 229910002651 NO3 Inorganic materials 0.000 description 1
- NHNBFGGVMKEFGY-UHFFFAOYSA-N Nitrate Chemical compound [O-][N+]([O-])=O NHNBFGGVMKEFGY-UHFFFAOYSA-N 0.000 description 1
- XLKNMWIXNFVJRR-UHFFFAOYSA-N boron potassium Chemical compound [B].[K] XLKNMWIXNFVJRR-UHFFFAOYSA-N 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/0819—Primers or igniters for the initiation of rocket motors, i.e. pyrotechnical aspects thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/10—Percussion caps
Definitions
- Leonard Flank and Charles R. Carter ABSTRACT A nonelectric squib assembly consisting of a squib body and a firing mechanism housing.
- the squib body includes a metallic seal separating a firing mechanism in the housing from a percussion primer in the squib body.
- the primary feature of the metallic seal is that it prevents missile motor pressure from producing a path for gases to flow back through the entire assembly.
- the metallic seal is dented by the firing mechanism to activate the primer thereby permitting primer gases to ignite a charge of boron-potassium nitrate carried in the squib body, which in turn is used to initiate the motor ignitor.
- the present invention provides a solution to this problem by providing a nonelectric squib which offers less hazard to operating personnel and property than the electric squib yet performs all the functions required of an electric squib.
- This perfon'nance is accomplished by a metallic seal that prevents missile motor pressure from producing a path for gases of flow back through the entire assembly.
- the seal also allows the use of a small charge to drive a firing pin to dent the seal and thereby initiate the squib. Final arming is performed external to the missile and late in the countdown thus reducing exposure of personnel to hazard.
- FIGURE shown in the drawing is a sectional perspective view of the nonelectric squib.
- Reference numeral 1 indicates generally the nonelectric squib assembly.
- a firing mechanism housing 2 is shown in axial alignment with and attached at one end of a squib body and houses a small booster charge (not shown). The firing mechanism is secured to the squib body to complete final anning of the missile.
- a shear pin 3 holds a piston-type firing pin 4 until the booster charge forces pin 4 thus shearing pin 3 and allowing pin 4 to slidably move forward.
- the firing pin has an operating contact point 4:
- the squib body includes a first chamber 6 housing a percussion primer 7.
- a seal 8 is in a thin disc made of metal, such as copper,'and is attached in a position so that one side thereof is adjacent contact point 4 and the opposite side of the seal closes off one end of chamber 6.
- An inner disc 9 is made of aluminum foil and located at the opposite end of chamber 6 separating this chamber from one end of a second chamber 10.
- the primer in chamber 6, when activated, will emit gases that will rupture disc 9 and thereby enter chamber 10 which contains an igniter charge such as boron-potassium nitrate (B-KNO identified by reference numeral II.
- a composite disc 12 at the opposite end of chamber 10 is a combination made up of a mica disc 13 and a mild steel disc I4. After the igniter charge is ignited, composite disc 12 ruptures to allow the output of the igniter charge to initiate the motor ignitor.
- a detonation wave is transmitted to the booster charge in the firing mechanism housing, the charge ignites and drives the firing pin forward shearing the shear pin.
- the contact point of the firing pin dents the metallic seal to activate the percussion primer.
- the primer gases rupture the inner disc and the gases are emitted into the chamber containing the igniter charge such as boronpotassium nitrate which in turn is ignited.
- the output of the igniter charge ruptures the composite disc and is then used to initiate the motor igniter.
- a nonelectric squib assembly for igniting a missile motor and for preventing gas flowback through the assembly comprising: a squib body having a firing mechanism housing at one end thereof, a first chamber and a second chamber; a filing pin mounted for slidable movement within said squib body, said firing pin having a contact point on one end thereof; a shear pin connected between said squib body and said firing pin to restrain movement of said firing pin until squib operation is started; a metallic seal disposed between said contact point and one end of said first chamber for hennetically sealing the firing pin from gases flowing back when the missile motor is ignited; a percussion primer disposed in said first chamber adjacent said metallic seal; a rupturable inner disc of aluminum foil separating said first chamber from said second chamber and sensitive to gaseous pressures from said primer; a missile motor igniter charge disposed in said second chamber; and a composite disc consisting of mica and mild steel discs at the opposite end of said second chamber for separation of said squib
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Air Bags (AREA)
Abstract
A nonelectric squib assembly consisting of a squib body and a firing mechanism housing. The squib body includes a metallic seal separating a firing mechanism in the housing from a percussion primer in the squib body. The primary feature of the metallic seal is that it prevents missile motor pressure from producing a path for gases to flow back through the entire assembly. The metallic seal is dented by the firing mechanism to activate the primer thereby permitting primer gases to ignite a charge of boron-potassium nitrate carried in the squib body, which in turn is used to initiate the motor ignitor.
Description
United States Patent [7 2] Inventor Rudolph E. Nett Los Angeles, Calif. [21] Appl. No. 823,351 [22] Filed May 9, 1969 [45] Patented Oct. 5, 1971 [73] Assignee The United States of America as represented by the Secretary of the Army [54] NONELECTRIC SQUIB ASSEMBLY 1 Claim, 1 Drawing Fig. I [52] US. Cl 102/29 [51] Int. Cl. F42c 15/06 [50] Field of Search 102/27, 29, 45,497, 70, 86.5, DIG. 1
[56] References Cited UNITED STATES PATENTS 3,114,290 12/1963 Harvey et al 102/DlG. 1
3,129,663 4/1964 Schnepfe,.lr. 102/27 3,274,937 9/1966 Kyle l02/28X Primary Examiner-Verlin R. Pendegrass Attorneys-William G. Gapcynski, Lawrence A. Neureither,
Leonard Flank and Charles R. Carter ABSTRACT: A nonelectric squib assembly consisting of a squib body and a firing mechanism housing. The squib body includes a metallic seal separating a firing mechanism in the housing from a percussion primer in the squib body. The primary feature of the metallic seal is that it prevents missile motor pressure from producing a path for gases to flow back through the entire assembly. The metallic seal is dented by the firing mechanism to activate the primer thereby permitting primer gases to ignite a charge of boron-potassium nitrate carried in the squib body, which in turn is used to initiate the motor ignitor.
PATENTEU Gm 519?: 3,610,151
Rudolph E. Nefl INVENTOR NONELECTRIC SQUIB ASSEMBLY BACKGROUND OF THE INVENTION SUMMARY OF THE INVENTION The present invention provides a solution to this problem by providing a nonelectric squib which offers less hazard to operating personnel and property than the electric squib yet performs all the functions required of an electric squib. This perfon'nance is accomplished by a metallic seal that prevents missile motor pressure from producing a path for gases of flow back through the entire assembly. The seal also allows the use of a small charge to drive a firing pin to dent the seal and thereby initiate the squib. Final arming is performed external to the missile and late in the countdown thus reducing exposure of personnel to hazard.
This invention may be better understood from the following detailed description taken in conjunction with the accompanying drawing.
BRIEF DESCRIPTION OF THE DRAWING The single FIGURE shown in the drawing is a sectional perspective view of the nonelectric squib.
PREFERRED EMBODIMENT OF THE INVENTION Reference numeral 1 indicates generally the nonelectric squib assembly. A firing mechanism housing 2 is shown in axial alignment with and attached at one end of a squib body and houses a small booster charge (not shown). The firing mechanism is secured to the squib body to complete final anning of the missile. A shear pin 3 holds a piston-type firing pin 4 until the booster charge forces pin 4 thus shearing pin 3 and allowing pin 4 to slidably move forward. The firing pin has an operating contact point 4: The squib body includes a first chamber 6 housing a percussion primer 7. A seal 8 is in a thin disc made of metal, such as copper,'and is attached in a position so that one side thereof is adjacent contact point 4 and the opposite side of the seal closes off one end of chamber 6.
This seal does not rupture when dented by contact point 4 and thus provides a hermetic seal for the squib body. The seal also prevents missile motor pressure from producing a path for gases to flow back through the entire assembly. An inner disc 9 is made of aluminum foil and located at the opposite end of chamber 6 separating this chamber from one end of a second chamber 10. The primer in chamber 6, when activated, will emit gases that will rupture disc 9 and thereby enter chamber 10 which contains an igniter charge such as boron-potassium nitrate (B-KNO identified by reference numeral II. A composite disc 12 at the opposite end of chamber 10 is a combination made up of a mica disc 13 and a mild steel disc I4. After the igniter charge is ignited, composite disc 12 ruptures to allow the output of the igniter charge to initiate the motor ignitor.
In operation a detonation wave is transmitted to the booster charge in the firing mechanism housing, the charge ignites and drives the firing pin forward shearing the shear pin. The contact point of the firing pin dents the metallic seal to activate the percussion primer. Alter the primer has been activated the primer gases rupture the inner disc and the gases are emitted into the chamber containing the igniter charge such as boronpotassium nitrate which in turn is ignited. The output of the igniter charge ruptures the composite disc and is then used to initiate the motor igniter.
I claim:
1. A nonelectric squib assembly for igniting a missile motor and for preventing gas flowback through the assembly comprising: a squib body having a firing mechanism housing at one end thereof, a first chamber and a second chamber; a filing pin mounted for slidable movement within said squib body, said firing pin having a contact point on one end thereof; a shear pin connected between said squib body and said firing pin to restrain movement of said firing pin until squib operation is started; a metallic seal disposed between said contact point and one end of said first chamber for hennetically sealing the firing pin from gases flowing back when the missile motor is ignited; a percussion primer disposed in said first chamber adjacent said metallic seal; a rupturable inner disc of aluminum foil separating said first chamber from said second chamber and sensitive to gaseous pressures from said primer; a missile motor igniter charge disposed in said second chamber; and a composite disc consisting of mica and mild steel discs at the opposite end of said second chamber for separation of said squib ignition from the missile motor, whereby missile motor pressure is prevented from producing a path for motor gases to flow back through the entire squib assembly.
Claims (1)
1. A nonelectric squib assembly for igniting a missile motor and for preventing gas flowback through the assembly comprising: a squib body having a firing mechanism housing at one end thereof, a first chamber and a second chamber; a firing pin mounted for slidable movement within said squib body, said firing pin having a contact point on one end thereof; a shear pin connected between said squib body and said firing pin to restrain movement of said firing pin until squib operation is started; a metallic seal disposed between said contact point and one end of said first chamber for hermetically sealing the firing pin from gases flowing back when the missile motor is ignited; a percussion primer disposed in said first chamber adjacent said metallic seal; a rupturable inner disc of aluminum foil separating said first chamber from said second chamber and sensitive to gaseous pressures from said primer; a missile motor igniter charge disposed in said second chamber; and a composite disc consisting of mica and mild steel discs at the opposite end of said second chamber for separation of said squib ignition from the missile motor, whereby missile motor pressure is prevented from producing a path for motor gases to flow back through the entire squib assembly.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US82335169A | 1969-05-09 | 1969-05-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3610151A true US3610151A (en) | 1971-10-05 |
Family
ID=25238510
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US823351A Expired - Lifetime US3610151A (en) | 1969-05-09 | 1969-05-09 | Nonelectric squib assembly |
Country Status (1)
Country | Link |
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US (1) | US3610151A (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3789761A (en) * | 1973-02-02 | 1974-02-05 | Us Army | Propagation transfer arrangement |
FR2392357A1 (en) * | 1977-05-27 | 1978-12-22 | Rheinmetall Gmbh | PROPULSIVE CHARGING IGNITER FOR CARTRIDGES WITHOUT SOCKET OF AMMUNITION TO BE CHARGED SEPARATE ELEMENTS |
US4265177A (en) * | 1978-04-07 | 1981-05-05 | Nitro Nobel Ab | Device in blasting cap for low-energy fuse |
EP0040011A1 (en) * | 1980-05-09 | 1981-11-18 | EMI Limited | Arrangements for igniting a pyrotechnic charge |
EP0122012A2 (en) * | 1983-04-08 | 1984-10-17 | Ici Americas Inc. | Impact sensitive high temperature detonator |
US4612857A (en) * | 1984-07-16 | 1986-09-23 | Mcdonnell Douglas Corporation | Ballistic gas fired device |
US20160102030A1 (en) * | 2014-09-10 | 2016-04-14 | University Of Central Florida Research Foundation Inc. | Primer for Firearms and Other Munitions |
US20160202033A1 (en) * | 2013-08-26 | 2016-07-14 | Dynaenergetics Gmbh & Co. Kg | Ballistic transfer module |
EP3527929A1 (en) * | 2018-02-15 | 2019-08-21 | Goodrich Corporation | High explosive firing mechanism |
US20220049936A1 (en) * | 2020-08-11 | 2022-02-17 | Detotec North America | Non-electric initiator system |
US11650037B2 (en) | 2021-02-16 | 2023-05-16 | Spectre Materials Sciences, Inc. | Primer for firearms and other munitions |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3114290A (en) * | 1962-10-12 | 1963-12-17 | Earle M Harvey | Breech sealing means for automatic firearms adapted to fire caseless ammunition |
US3129663A (en) * | 1961-08-11 | 1964-04-21 | Aircraft Armaments Inc | Fittings for low energy detonating cord |
US3274937A (en) * | 1963-04-11 | 1966-09-27 | Physical Sciences Corp | Detonation squib |
-
1969
- 1969-05-09 US US823351A patent/US3610151A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3129663A (en) * | 1961-08-11 | 1964-04-21 | Aircraft Armaments Inc | Fittings for low energy detonating cord |
US3114290A (en) * | 1962-10-12 | 1963-12-17 | Earle M Harvey | Breech sealing means for automatic firearms adapted to fire caseless ammunition |
US3274937A (en) * | 1963-04-11 | 1966-09-27 | Physical Sciences Corp | Detonation squib |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3789761A (en) * | 1973-02-02 | 1974-02-05 | Us Army | Propagation transfer arrangement |
FR2392357A1 (en) * | 1977-05-27 | 1978-12-22 | Rheinmetall Gmbh | PROPULSIVE CHARGING IGNITER FOR CARTRIDGES WITHOUT SOCKET OF AMMUNITION TO BE CHARGED SEPARATE ELEMENTS |
US4265177A (en) * | 1978-04-07 | 1981-05-05 | Nitro Nobel Ab | Device in blasting cap for low-energy fuse |
EP0040011A1 (en) * | 1980-05-09 | 1981-11-18 | EMI Limited | Arrangements for igniting a pyrotechnic charge |
US4541342A (en) * | 1980-05-09 | 1985-09-17 | Emi Limited | Pyrotechnic device with metal diaphragm and metal insert |
EP0122012A2 (en) * | 1983-04-08 | 1984-10-17 | Ici Americas Inc. | Impact sensitive high temperature detonator |
EP0122012A3 (en) * | 1983-04-08 | 1985-10-16 | Ici Americas Inc | Impact sensitive high temperature detonator |
US4612857A (en) * | 1984-07-16 | 1986-09-23 | Mcdonnell Douglas Corporation | Ballistic gas fired device |
US9988885B1 (en) | 2013-08-26 | 2018-06-05 | Dynaenergetics Gmbh & Co. Kg | Method of initiating a percussion initiator |
US20160202033A1 (en) * | 2013-08-26 | 2016-07-14 | Dynaenergetics Gmbh & Co. Kg | Ballistic transfer module |
US9890619B2 (en) * | 2013-08-26 | 2018-02-13 | Dynaenergetics Gmbh & Co.Kg | Ballistic transfer module |
US20160102030A1 (en) * | 2014-09-10 | 2016-04-14 | University Of Central Florida Research Foundation Inc. | Primer for Firearms and Other Munitions |
US10882799B2 (en) * | 2014-09-10 | 2021-01-05 | Spectre Materials Sciences, Inc. | Primer for firearms and other munitions |
EP3527929A1 (en) * | 2018-02-15 | 2019-08-21 | Goodrich Corporation | High explosive firing mechanism |
US10837747B2 (en) | 2018-02-15 | 2020-11-17 | Goodrich Corporation | High explosive firing mechanism |
US20220049936A1 (en) * | 2020-08-11 | 2022-02-17 | Detotec North America | Non-electric initiator system |
US11892277B2 (en) * | 2020-08-11 | 2024-02-06 | Detotec North America | Non-electric initiator system |
US11650037B2 (en) | 2021-02-16 | 2023-05-16 | Spectre Materials Sciences, Inc. | Primer for firearms and other munitions |
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