US2942547A - Gas generating assembly - Google Patents

Gas generating assembly Download PDF

Info

Publication number
US2942547A
US2942547A US744253A US74425358A US2942547A US 2942547 A US2942547 A US 2942547A US 744253 A US744253 A US 744253A US 74425358 A US74425358 A US 74425358A US 2942547 A US2942547 A US 2942547A
Authority
US
United States
Prior art keywords
gas generating
ignition
cartridge
charge
grain
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
Application number
US744253A
Other languages
English (en)
Inventor
Rabern Joseph William
Norman J Wilkaitis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Olin Corp
Original Assignee
Olin Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Olin Corp filed Critical Olin Corp
Priority to US744253A priority Critical patent/US2942547A/en
Priority to GB21145/59A priority patent/GB861622A/en
Priority to BE579979A priority patent/BE579979A/fr
Priority to CH7485659A priority patent/CH376321A/de
Priority to FR798438A priority patent/FR1228673A/fr
Priority to DEO6844A priority patent/DE1109577B/de
Application granted granted Critical
Publication of US2942547A publication Critical patent/US2942547A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • F42B3/04—Blasting cartridges, i.e. case and explosive for producing gas under pressure
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
    • C06C9/00—Chemical contact igniters; Chemical lighters

Definitions

  • This invention relates to gas gen'erating'units and par ticularly to improved ignition assemblies therefor.
  • Solid gas generating charges are generally. used as the source of power for the operation of prime movers such as internal combustion engines, motor starters, switch closers, jet engine starters, and" the like.
  • Ain'- monium nitrate with plastic binders has been regarded as the most suitable gas generating material in such charges because of its low cost, ease and safety in handling, and the predictability and control of gases generated upon ignition.
  • ammonium nitrate consolidated charges are exceedingly difiicult to ignite. Therefore, previous attempts to utilize ammonium nitrate in sol-id gas generating charges has not been completely satisfactory because no reliable means has heretofore been found for their ignition.
  • such solid gas generating charges develop gas and pressure in a more or less step- Wise manner.
  • the initial power generation must be suiti'ciently great to overcome the inertia of the driven mechanism but at the same time not so great as to destroy the mechanism or subject it'to undue mechanical force before his put in motion.
  • the power demands from the gas generating charge are much greater.
  • Prior art generating devices have been quite deficient in their capability of providing a relatively low pressure followed by a sustained substantially constant higher pressure, and this recognized desirable result could not be reproduceably obtained. 4 v
  • an object of this invention to provide a gas generating cartridge and an ignition means therefor overcoming the disadvantages of the prior art.
  • Another object of this invention is to provide an improved ignition assembly for solid gas generating charges.
  • a more specific'object of this invention is to provide a solid gas generating assembly capable of reliably igniting am monium nitrate type gas generating charges as well as other types of gas generating charges in a stepwise manner.
  • Figure 1 is a longitudinal sectional view of a gas generatingcartridge illustrating a preferred embodiment of the present invention.
  • ' Figure 2 is a transverse view partially in section taken along'the' lines IIII of Figure 1.
  • the present invention contemplates a cylindrical consolidated gas generating charge or grain provided with a centrally located longitudinal perforation and an ignition system for the grain;
  • One portion of the Patented June 28, 1960 ignition system for the grain consists of a consolidated ignition or pyrotechnic charge located within the perforationof the grain and near the discharge port.
  • an electric squib imbedded in an igniter assembly is centrally positioned at the other end of the perforation and a plurality of auxiliary ignition pellets are provided below the'main fuel charge near the closed end of the cartridge.
  • the gas generating charge of the present invention is preferably contained in a resilient casing which is adapted upon ignition of the charge to expand so as to effectively seal the breech structure or other mechanism in which the cartridge is fired.
  • a resilient casing which is adapted upon ignition of the charge to expand so as to effectively seal the breech structure or other mechanism in which the cartridge is fired.
  • Various types of synthetic rubber and elastomers can be used in this connection.
  • organic casing it is preferably provided with'a'n insulating lining such as asbestos or the like and also with a reinforcing lining of metal or other suitable material.
  • a metallic casing can be used. One end ofthe casing is closed and'carries the necessary electrical contacts, while the opposite end constitutes the discharge port.
  • the discharge end is spanned by a screen or a perforated metal plate to permit passage of the gases interior of the chamber but is of a slightly smaller diatrn. eter' so as to provide an annular space about the periphcry of the grain.
  • This annular space which is essential for'theproper combustion of the grain, is maintained by any suitable spacing means.
  • the end surfaces of the ammonium nitrate charge are inhibited by any converttional means to prevent end burning.
  • a layer of a non-combustible material such as rubber-asbestos, am: monium oxalate-synthetic rubber, epoxy resins, polyurethane, or the like, can be afiixed to the end surfaces of the grain for this purpose.
  • the ignition stimulus for the system originates from an electric squib or similar deflagrating device embedded in a body of a vigorous ignition composition.
  • This ignition composition in which the squib is embedded is preferably contained in a plastic cup which, upon ignition, disintegrates without forming any harmfulresidue. While polyethylene is particularly well suited for this purpose, any other suitably evanescent material can be used.
  • the plastic cup is centrally located near the closed end of the cartridge and is aligned with the central perforation of the main fuel charge.
  • the top of the cup is provided witht a closure that will readily yield upon ignition of :the contents of the cup.
  • the top portion of the cup is directed into the central perforation of the grain and preferably extends partially thereinto:
  • top is applied'to the discharge end of the cartridge and the term bottom is applied to the closed end. It will, of course; be readily apparent that this cartridge can be fired in any position.
  • compositions capable of pro ducing an intense flame with a moderate evolutionof gaseous products can be'utilized in this plastic cup. These charges are preferably provided with a binder; Compositions containing'a metal, a plastic binder, and an oxidizer are particularly well suited for this purpose. .Co'mposie tions containing polyvinyl acetate, boron, and potassium perchlorate have been found to be satisfactory but'othei 3 metals, including aluminum and the like, fuels and oxidizers can, of course, be used.
  • the ignition composition contained in the plastic cup is augmentedby anignition pellet located in the central perforation of the grain remote from the squib and a plurality of cakes of fast burning propellent located about the plastic cup at the closed end of the cartridge.
  • auxiliary ignition cake charges are preferably a composi-, tion made with a rubber type binder, similar to a fast burning rocket propellent.
  • the pellet ignition charge positioned within the perforation of the grain is preferably contained in a plastic holder and is provided with an inhibitor to restrict burning on the cylindrical surface 4 a of the pellet except for a portion near the open end of the plastic holder.
  • the body of the cartridge consists of a synthetic rubber casing :1, the sidewalls of which are provided with a liner 2 of asbestos and a metallic reinforcing liner 3.
  • the closed end of the cartridge is dome shaped, as indicated generally at 4 and the opposing discharge end is closed by a perforated plate or screen 5, which is crimped about the lower end of the cartridge as shown at 6.
  • a thin layer 7 of polyester plastic tape or other evanescent plastic material is positioned over screen to provide a weather seal for the cartridge.
  • the main fuel charge is a consolidated grain 8 of granular ammonium nitrate in a binder of polybutadiene acrylic acid type synthetic rubber.
  • This grain is provided with a layer of inhibitor 23 at each end to insure lateral burning.
  • the grain is maintained in position within the cartridge by plastic spacers 9 which are integral with lateral extensions 10 of centrally located support 11.
  • Metallic supports 12 cooperate with plastic members 9 to maintain the grain in alignment. These members extend from the central portion of the closed end of the cartridge to the top of the gas generating grain.
  • the electrical contacts forinitiation of the squib pass through the closed end of the cartridge and are shown generally at 13.
  • Squib 14 is provided with lead wires 15 and is embedded in a black powder-pyrotechnic mixture 16 having the following approximate composition:
  • the assembly is also provided with four cast propellent charges or cakes 22 which are bonded to supporting members 12 and positioned radially toplastic cup 17 between the main grain and the closed end of the cartridge.
  • Two of these four pressed charges were composed of a mixture of about 75.0% ammonium perchlorate, 12.5% polyvinyl chloride, and 12.5% dioctyl phthalate, while the remaining two charges were composed of boron aluminum potassium perchlorate graphite polyvinyl acetate fully explain and clarify the in a mixture of about 57.5% potassium perchlorate, 12.5% aluminum powder, 5% boron, 12.5% dioctyl phthalate, and 12.5 polyvinyl chloride.
  • the remaining two cast propellent cakes can be composed of a mixture of about 12.5% dioctyl phthalate, 12.5% polyvinyl chloride, 1% boron, and 74% potassium perchlorate.
  • squib 14 Upon firing the cartridge, squib 14 ignites ignition charge 16 whose flame is directed through the central perforation of the gas generating charge so as to impinge upon the exposed surface of igniter pellet 20. Charge 20 then ignites vigorously and together with the action of charge 16 initiates combustion of the gas generating charge 8 on its surface on the central perforation 19. Auxiliary ignition charges 22 are then ignited and assist in carrying the flame and hot gases to the peripheral surfaces of the ammonium nitrate grain.
  • the elastomeric case '1 is readily expanded so as to avoid any gas leakage or blow-back in the breech mechanism or cartridge holder which is not shown and does not form a part of the present invention.
  • the plastic covering 7 for the foraminous closure plate 5 ruptures or burns so as to provide ready egress for the gaseous combustion products.
  • the ignition of the main gas generating charge in its central perforation by substantially non-gaseous ignition charges followed by ignition of the outer surface of the grain provides 'a system wherein the initial pressure generated by the cartridge is relatively low and is followed by a sustained period of substantially high pressure generation.
  • a gas generating cartridge for an engine starter and the like comprising a substantially cylindrical resilient casing having a permanently closed end and an oppositely disposed discharge end, a centrally perforated substantially cylindrical end-inhibited ammonium nitrate gas generating charge disposed in and spaced from the casing as the main charge, the longitudinal axes of the cylindrical casing and of the cylindrical gas generating charge being substantially parallel, a laterally and basally inhibited cylindrical pyrotechnic charge positioned in and substantially filling that portion of the central perforation proximate the discharge end of the cartridge, the base of the pyrotechinc charge being proximate the discharge end of the cartridge, an electric squib embedded in an ignition mixture, said ignition mixture being contained in an evanescent plastic cup positioned at the closed end of the cartridge and having'a portion extending into and substantially closing that portion of the central perforation proximate the closed end of the cartridge, and a plurality of ignition charges positioned radially about the plastic cup and between the closed end of the cartridge and
  • a gas generating cartridge for an engine starter and the like comprising a substantially cylindrical resilient casing having a permanently closed end and an oppositely disposed discharge end, an end inhibited gas generating centrally perforated grain contained in the casing and spaced therefrom, an evanescent cup positioned at one end of the perforation with a cylindrical portion of the cup extending into and closing that end of the perforation, the evanescent cup containing an ignition mixture having an electric squib embedded therein, the opposite end of the perforation being closed by a pyrotechnic charge free to burn only on that surface facing the evanescent cup, and a plurality of ignition charges positioned radially about the plastic cup and between the closed end of the cartridge and the gas generating grain.
  • a fuel charge for a gas generating device comprising as the main fuel a cylindrical end-inhibited grain of a gas generating composition having at least one longitudinal perforation, a laterally and basally inhibited cylindrical pyrotechnic charge substantially filling one end of the perforation in the gas generating charge, the top of the pyrotechnic charge extending into the perforation, an ignition assembly closing the other end of the perforation and containing an electric squib embedded in an ignitor mixture contained in an evanescent plastic cup, a plurality of ignition charges positioned radially about the ignition assembly and between the perforation and the external wall of the cylindrical grain, and means supporting said grain and charges.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Lighters Containing Fuel (AREA)
US744253A 1958-06-24 1958-06-24 Gas generating assembly Expired - Lifetime US2942547A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US744253A US2942547A (en) 1958-06-24 1958-06-24 Gas generating assembly
GB21145/59A GB861622A (en) 1958-06-24 1959-06-19 Improvements in or relating to gas generating devices
BE579979A BE579979A (fr) 1958-06-24 1959-06-23 Perfectionnements aux dispositifs générateurs de gaz
CH7485659A CH376321A (de) 1958-06-24 1959-06-24 Brennstoffpatrone für Gaserzeugungsvorrichtungen, insbesondere zum Anlassen von Kraftmaschinen
FR798438A FR1228673A (fr) 1958-06-24 1959-06-24 Dispositif générateur de gaz
DEO6844A DE1109577B (de) 1958-06-24 1959-06-24 Brennstoffladung fuer eine Vorrichtung zur Gaserzeugung

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US744253A US2942547A (en) 1958-06-24 1958-06-24 Gas generating assembly

Publications (1)

Publication Number Publication Date
US2942547A true US2942547A (en) 1960-06-28

Family

ID=24992038

Family Applications (1)

Application Number Title Priority Date Filing Date
US744253A Expired - Lifetime US2942547A (en) 1958-06-24 1958-06-24 Gas generating assembly

Country Status (6)

Country Link
US (1) US2942547A (de)
BE (1) BE579979A (de)
CH (1) CH376321A (de)
DE (1) DE1109577B (de)
FR (1) FR1228673A (de)
GB (1) GB861622A (de)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3069845A (en) * 1958-03-14 1962-12-25 Mini Of Supply Liner for cooling rocket motors
US3077077A (en) * 1959-07-01 1963-02-12 Honeywell Regulator Co Solid propellant pressurizing device
US3138927A (en) * 1962-07-18 1964-06-30 North American Aviation Inc Gas generator
US3148505A (en) * 1960-01-04 1964-09-15 North American Aviation Inc Radially firing pyrotechnic igniter
US3236317A (en) * 1962-07-02 1966-02-22 Dresser Ind Projectile propelling apparatus for use in high temperature environment
US3294020A (en) * 1964-01-24 1966-12-27 Dynamit Nobel Ag Ignition device
US3375656A (en) * 1966-07-01 1968-04-02 Thiokol Chemical Corp Gas generator cartridge
US3446017A (en) * 1966-11-22 1969-05-27 Olin Mathieson Fail-safe switch for gas generator
US3516797A (en) * 1967-04-03 1970-06-23 Automatic Sprinkler Corp Chemical oxygen generator
US3572040A (en) * 1969-03-06 1971-03-23 Messerschmitt Boelkow Blohm Solid fuel gas generator
US3641935A (en) * 1969-06-23 1972-02-15 Dynamit Nobel Ag Pressure cartridge containing solid fuel propellant charge
US3719040A (en) * 1968-04-30 1973-03-06 Messerschmitt Boelkow Blohm Gas generator and tubular solid charge construction therefore
US4498292A (en) * 1983-02-02 1985-02-12 Thiokol Corporation Igniter for rocket motors
US4658578A (en) * 1984-01-10 1987-04-21 Morton Thiokol Inc. Igniting rocket propellants under vacuum conditions
WO1999000275A1 (en) * 1997-06-27 1999-01-07 Atlantic Research Corporation Tailorable output electrically activated gasgenerating device

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1771943C2 (de) * 1968-08-05 1975-03-27 Dynamit Nobel Ag, 5210 Troisdorf Anfeuerungssatz für Treibladungen und Raketentreibsätze
US3620683A (en) * 1968-11-14 1971-11-16 Ato Inc Gas generator
US3607122A (en) * 1969-01-14 1971-09-21 Ato Inc Gas generator housing
RU2627409C1 (ru) * 2016-02-16 2017-08-08 Федеральное казенное предприятие "Государственный научно-исследовательский институт химических продуктов" (ФКП "ГосНИИХП") Воспламенительный состав

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE502757C (de) * 1930-08-05 Pyrotechnische Fabriken Akt Ge Verfahren zur Entzuendung schwer verbrennlicher Reaktionsgemische, insbesondere fuer Brennkraftmaschinen
US2518958A (en) * 1945-06-20 1950-08-15 Ici Ltd Electrically ignitible power gas generating blank cartridges
US2685837A (en) * 1943-04-02 1954-08-10 Us Navy Igniter
US2688920A (en) * 1952-07-24 1954-09-14 Ici Ltd Gas generating cartridge
US2743580A (en) * 1952-10-07 1956-05-01 Hughes Aircraft Co Igniter for rocket motors
US2771035A (en) * 1953-03-05 1956-11-20 Olin Mathieson Propellant
US2865456A (en) * 1956-08-22 1958-12-23 Specialties Dev Corp Pressurizing cartridge and pyrotechnic charge therefor

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1099904A (fr) * 1949-08-03 1955-09-14 Perfectionnements aux procédés et aux dispositifs pour la production des gaz sous pression
BE511319A (de) * 1951-05-11
FR1077744A (fr) * 1952-05-07 1954-11-10 Ici Ltd Charges dégageant des gaz et cartouches les contenant

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE502757C (de) * 1930-08-05 Pyrotechnische Fabriken Akt Ge Verfahren zur Entzuendung schwer verbrennlicher Reaktionsgemische, insbesondere fuer Brennkraftmaschinen
US2685837A (en) * 1943-04-02 1954-08-10 Us Navy Igniter
US2518958A (en) * 1945-06-20 1950-08-15 Ici Ltd Electrically ignitible power gas generating blank cartridges
US2688920A (en) * 1952-07-24 1954-09-14 Ici Ltd Gas generating cartridge
US2743580A (en) * 1952-10-07 1956-05-01 Hughes Aircraft Co Igniter for rocket motors
US2771035A (en) * 1953-03-05 1956-11-20 Olin Mathieson Propellant
US2865456A (en) * 1956-08-22 1958-12-23 Specialties Dev Corp Pressurizing cartridge and pyrotechnic charge therefor

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3069845A (en) * 1958-03-14 1962-12-25 Mini Of Supply Liner for cooling rocket motors
US3077077A (en) * 1959-07-01 1963-02-12 Honeywell Regulator Co Solid propellant pressurizing device
US3148505A (en) * 1960-01-04 1964-09-15 North American Aviation Inc Radially firing pyrotechnic igniter
US3236317A (en) * 1962-07-02 1966-02-22 Dresser Ind Projectile propelling apparatus for use in high temperature environment
US3138927A (en) * 1962-07-18 1964-06-30 North American Aviation Inc Gas generator
US3294020A (en) * 1964-01-24 1966-12-27 Dynamit Nobel Ag Ignition device
US3375656A (en) * 1966-07-01 1968-04-02 Thiokol Chemical Corp Gas generator cartridge
US3446017A (en) * 1966-11-22 1969-05-27 Olin Mathieson Fail-safe switch for gas generator
US3516797A (en) * 1967-04-03 1970-06-23 Automatic Sprinkler Corp Chemical oxygen generator
US3719040A (en) * 1968-04-30 1973-03-06 Messerschmitt Boelkow Blohm Gas generator and tubular solid charge construction therefore
US3572040A (en) * 1969-03-06 1971-03-23 Messerschmitt Boelkow Blohm Solid fuel gas generator
US3641935A (en) * 1969-06-23 1972-02-15 Dynamit Nobel Ag Pressure cartridge containing solid fuel propellant charge
US4498292A (en) * 1983-02-02 1985-02-12 Thiokol Corporation Igniter for rocket motors
US4658578A (en) * 1984-01-10 1987-04-21 Morton Thiokol Inc. Igniting rocket propellants under vacuum conditions
WO1999000275A1 (en) * 1997-06-27 1999-01-07 Atlantic Research Corporation Tailorable output electrically activated gasgenerating device

Also Published As

Publication number Publication date
GB861622A (en) 1961-02-22
DE1109577B (de) 1961-06-22
BE579979A (fr) 1959-12-23
FR1228673A (fr) 1960-08-31
CH376321A (de) 1964-03-31

Similar Documents

Publication Publication Date Title
US2942547A (en) Gas generating assembly
US3062147A (en) Igniter for solid propellant grains
US2703960A (en) Rocket
US2195965A (en) Gas producing cartridge
US2984973A (en) Liquid-solid bipropellant rocket
US3982488A (en) Flueric through bulkhead rocket motor ignitor
US2597641A (en) Pressure-operated starting device
US2309978A (en) Propellent fuel assembly
GB1229119A (de)
US3771451A (en) Low pressure ballistic system
US2743580A (en) Igniter for rocket motors
GB1428412A (en) Solid fuel rocket motors
US3701256A (en) Demand, solid-propellant gas generator
US2974484A (en) Ignition system for rocket motors
US2289318A (en) Propellent fuel cartridge
US3129561A (en) Rocket engine igniter
US2973713A (en) Ignition of solid rocket propellants
GB933349A (en) Improvements in or relating to projectiles
US3357190A (en) Device for igniting a combustible material
US4391196A (en) Add-on igniter for pyrogen type igniter
US3115007A (en) Self-actuating hybrid rocket motor
US3667396A (en) Solid propellant grain igniter
US3011441A (en) Igniter device
US2299464A (en) Power generating unit
US2455015A (en) Means for igniting propellant in rocket motors