US3519505A - Ignition material containing tellurium dioxide,boron and fluoropolymeric binder - Google Patents

Ignition material containing tellurium dioxide,boron and fluoropolymeric binder Download PDF

Info

Publication number
US3519505A
US3519505A US619567A US3519505DA US3519505A US 3519505 A US3519505 A US 3519505A US 619567 A US619567 A US 619567A US 3519505D A US3519505D A US 3519505DA US 3519505 A US3519505 A US 3519505A
Authority
US
United States
Prior art keywords
mixture
boron
tellurium dioxide
binder
material containing
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
US619567A
Inventor
Frank H Gardner
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.)
Space Ordnance Systems Inc
Original Assignee
Space Ordnance Systems Inc
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 Space Ordnance Systems Inc filed Critical Space Ordnance Systems Inc
Application granted granted Critical
Publication of US3519505A publication Critical patent/US3519505A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B43/00Compositions characterised by explosive or thermic constituents not provided for in groups C06B25/00 - C06B41/00
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B33/00Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide
    • C06B33/02Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide with an organic non-explosive or an organic non-thermic component

Definitions

  • a combustible material particularly suited for electrically initiated ordnance devices, consists of tellurium dioxide as the oxidizer and a fuel composed of boron and a fluoroelastomeric binder.
  • This invention relates to an initiating explosive mixture, such as is used in ordnance and quasi-ordnance devices. It is triggered by an electric bridge wire, or by any other means of rapidly raising the temperature to the ignition point, e.g. a laser beam. When fired, the initiator may be used in a number of ways, as by employing the resulting high pressure to rupture, fracture, or move a physical member, or by sudden heat generated to trigger another and larger combustible or explosive device.
  • Ignition or explosive mixtures of the type forming the subject matter of this invention are many and varied. They are customarily triggered or ignited by a sudden elevation in temperature as by current through a bridge Wire or more recently by energy from a laser beam.
  • One of the serious shortcomings of such explosive mixtures is that they are subject to unwanted triggering by uncontrolled electrostatic charges, high energy radio frequency signals, and other extraneously generated and applied electric current sources.
  • the mixture of the present invention is highly resistant to these random and uncontrollable electric currents because of its very high electric resistance. It responds normally, however, to high heat sources, such as are usually used to trigger devices of this sort, for example bridge wires and laser beams.
  • the present invention is essentially a non-conductive or very high resistance ignition mixture. It consists of tellurium dioxide as an oxidizer and a fuel consisting of boron and a binder.
  • the present invention consists preferably of a stoichiometric mixture of a fuel and an oxidizer.
  • the fuel comprises boron and a binder.
  • the preferred fluoroelastomeric binder is a copolymer of vinylidene fluoride and hexafluoropropylene marketed under the trademark Viton B by E. I. du Pont de Nemours & Co. having a repeating structure generally corresponding to the formula CF -CH CF CF(CF Its function is to give the mixture acceptable physical handling properties. It is also a fuel, however, and should be taken into account when determining the stoichiometric proportion of oxidizer.
  • the oxidizer is tellurium dioxide in powder form of 2 micronsil micron.
  • the boron is preferably elemental and non-compacted and has a particle size of approximately 300 angstroms.
  • the binder prior to being mixed into the compound, is dissolved in N-butyl acetate, which serves as a transient carrier that does not enter significantly into the ignition reaction. Most of it in fact evaporates during the compounding of the mixture.
  • acceptable ignition mixtures should lie somewhere close to a stoichiometric mixture between oxidizer and all fuel components. Either component, oxidizer or fuel, may vary as much as l0% from strict stoichiometric proportions and still produce an acceptable ignition material for the purposes of the present invention. When the fuel proportion is quite high, as for example up to 25% of the total mixture, the remaining being oxidizer (tellurium dioxide), the mixture is suited for use as a propellant in gas generators, rockets and the like.
  • the mixture of the present invention is preferably substantially stoichiometric, i.e. has the following composition by weight:
  • tellurium dioxide 88.4 parts:5% boron, 6.6 parts:t2% binder, 5.0 partsi2%
  • a stoichiometric mixture as specified immediately above has successfully withstood the discharge of 30,000 volts DC from a 500 picofarad capacitor, through a column of the mixture 0.87 inch long. The mixture did not fire or ignite, nor was it in any way damaged or deteriorated. It thereafter functioned properly, i.e. fired, when energized with a 3.5 ampere current pulse passing through a conventional bridge -wire embedded in the material.
  • the mixture of the present invention When assembled as an initiating charge in a conventional electric blasting cap, the mixture of the present invention has been tested With pulses of 60,000 volts from shorted circuit to case without causing uncontrolled firing or any damage or deterioration to the units. Thereafter, when heated by conventional bridge wires, such units fired properly.
  • a mixture of the present invention has been found to accept up to 670 F. without firing. This is about 250 F. higher than most of the commonly used initiating mix tures. This property of the present mixture reduces the heat shielding necessary in areas close to rocket propulsion chambers and nozzles. It also makes possible a reduction in heat shielding required in space capsule skin areas, which might be subject to heat due to air friction. This property also makes the mixture quite usable in deep oil wells where heat is a problem.
  • Use of the present mixture also improves confidence levels and reliabilities by allowing simple, straightforward initiator, igniter, and detonator designs, rather than requiring configurations with separate cavities for each circuit, special insulation barriers or bathtub-type cavities manufactured into a simple assembly header.
  • the present mixture by permitting elimination of metallic, electrostatic, and radio frequency shields, simplifies and ram ders more efiicient various missile and space craft designs.
  • Combustible mixture comprising: tellurium dioxide, and a fuel consisting of boron and a fluoroelastomeric binder, the portions of tellurium dioxide and fuel each being within plus or minus 10% of stoichiometric proportions.
  • fluoroelastomeric binder is a copolymer of vinylidene fluoride and hexafluoropropylene.
  • Combustible material comprising substantially tellurium dioxide and a fuel consisting of boron and a fluoroelastomeric binder mixed in the following proportions by weight:
  • tellurium dioxide 75 to 97 parts

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Air Bags (AREA)

Description

United States Patent IGNITION MATERIAL CONTAINING TELLURIUM DIOXIDE, BORON A'ND FLUOROPOLYMERIC BINDER Frank H. Gardner, Huntington Beach, Calif., assignor to Space Ordnance Systems, Inc., El Segundo, Calif., a corporation of California No Drawing. Filed Mar. 1, 1967, Ser. No. 619,567
Int. Cl. C06d /00 U.S. Cl. 149-19 4 Claims ABSTRACT OF THE DISCLOSURE A combustible material, particularly suited for electrically initiated ordnance devices, consists of tellurium dioxide as the oxidizer and a fuel composed of boron and a fluoroelastomeric binder.
BACKGROUND OF THE INVENTION This invention relates to an initiating explosive mixture, such as is used in ordnance and quasi-ordnance devices. It is triggered by an electric bridge wire, or by any other means of rapidly raising the temperature to the ignition point, e.g. a laser beam. When fired, the initiator may be used in a number of ways, as by employing the resulting high pressure to rupture, fracture, or move a physical member, or by sudden heat generated to trigger another and larger combustible or explosive device.
Ignition or explosive mixtures of the type forming the subject matter of this invention are many and varied. They are customarily triggered or ignited by a sudden elevation in temperature as by current through a bridge Wire or more recently by energy from a laser beam. One of the serious shortcomings of such explosive mixtures is that they are subject to unwanted triggering by uncontrolled electrostatic charges, high energy radio frequency signals, and other extraneously generated and applied electric current sources. The mixture of the present invention is highly resistant to these random and uncontrollable electric currents because of its very high electric resistance. It responds normally, however, to high heat sources, such as are usually used to trigger devices of this sort, for example bridge wires and laser beams.
SUMMARY The present invention is essentially a non-conductive or very high resistance ignition mixture. It consists of tellurium dioxide as an oxidizer and a fuel consisting of boron and a binder.
DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention consists preferably of a stoichiometric mixture of a fuel and an oxidizer. The fuel comprises boron and a binder.
The preferred fluoroelastomeric binder is a copolymer of vinylidene fluoride and hexafluoropropylene marketed under the trademark Viton B by E. I. du Pont de Nemours & Co. having a repeating structure generally corresponding to the formula CF -CH CF CF(CF Its function is to give the mixture acceptable physical handling properties. It is also a fuel, however, and should be taken into account when determining the stoichiometric proportion of oxidizer.
The oxidizer is tellurium dioxide in powder form of 2 micronsil micron.
The boron is preferably elemental and non-compacted and has a particle size of approximately 300 angstroms.
The binder, prior to being mixed into the compound, is dissolved in N-butyl acetate, which serves as a transient carrier that does not enter significantly into the ignition reaction. Most of it in fact evaporates during the compounding of the mixture.
In general it has been found that acceptable ignition mixtures should lie somewhere close to a stoichiometric mixture between oxidizer and all fuel components. Either component, oxidizer or fuel, may vary as much as l0% from strict stoichiometric proportions and still produce an acceptable ignition material for the purposes of the present invention. When the fuel proportion is quite high, as for example up to 25% of the total mixture, the remaining being oxidizer (tellurium dioxide), the mixture is suited for use as a propellant in gas generators, rockets and the like.
For use in initiator, ignition, and detonator devices, the mixture of the present invention is preferably substantially stoichiometric, i.e. has the following composition by weight:
tellurium dioxide, 88.4 parts:5% boron, 6.6 parts:t2% binder, 5.0 partsi2% A stoichiometric mixture as specified immediately above has successfully withstood the discharge of 30,000 volts DC from a 500 picofarad capacitor, through a column of the mixture 0.87 inch long. The mixture did not fire or ignite, nor was it in any way damaged or deteriorated. It thereafter functioned properly, i.e. fired, when energized with a 3.5 ampere current pulse passing through a conventional bridge -wire embedded in the material.
When assembled as an initiating charge in a conventional electric blasting cap, the mixture of the present invention has been tested With pulses of 60,000 volts from shorted circuit to case without causing uncontrolled firing or any damage or deterioration to the units. Thereafter, when heated by conventional bridge wires, such units fired properly.
The mixture when used in various physical firing cartridges has been subjected to radio frequencies in the x band up to 6 watts of energy without firing or being subjected to any deterioration. Radio frequency energies have been supplied directly through the mix from circuit to circuit and from shorted circuit to case. No firing or deterioration was noted and all units subsequently fired normally when subjected to normal bridge wire current.
A mixture of the present invention has been found to accept up to 670 F. without firing. This is about 250 F. higher than most of the commonly used initiating mix tures. This property of the present mixture reduces the heat shielding necessary in areas close to rocket propulsion chambers and nozzles. It also makes possible a reduction in heat shielding required in space capsule skin areas, which might be subject to heat due to air friction. This property also makes the mixture quite usable in deep oil wells where heat is a problem.
Use of the present mixture in known configurations of initiating devices eliminates the requirement for special and exotic physical designs now required to shield ignition mixtures from uncontrollable electric energies, such as discussed hereinbefore. It also allows redundancies to be accomplished by one simple system with two reliable circuits in one small device rather than two complete separate systems.
Use of the present mixture also improves confidence levels and reliabilities by allowing simple, straightforward initiator, igniter, and detonator designs, rather than requiring configurations with separate cavities for each circuit, special insulation barriers or bathtub-type cavities manufactured into a simple assembly header. The present mixture, by permitting elimination of metallic, electrostatic, and radio frequency shields, simplifies and ram ders more efiicient various missile and space craft designs.
Whereas the present invention has been shown and described herein in what is conceived to be the best'mode contemplated, it is recognized that departures may be made therefrom within the scope of the invention which is, therefore, not to be limited to the details disclosed herein, but is to be afforded the full scope of the invention as hereinafter claimed.
What is claimed is:
1. Combustible mixture comprising: tellurium dioxide, and a fuel consisting of boron and a fluoroelastomeric binder, the portions of tellurium dioxide and fuel each being within plus or minus 10% of stoichiometric proportions.
2. Mixture in accordance with claim 1, wherein said fluoroelastomeric binder is a copolymer of vinylidene fluoride and hexafluoropropylene.
3. Combustible material comprising substantially tellurium dioxide and a fuel consisting of boron and a fluoroelastomeric binder mixed in the following proportions by weight:
tellurium dioxide, 75 to 97 parts;
fuel, 10 to 25 parts.
References Cited UNITED STATES PATENTS 2,410,801 11/1946 Audrieth 14922 X 2,900,242 8/ 1959 Williams et al l4922 2,953,447 9/1960 Schulz 14937 2,988,438 6/1961 Allovio 149-43 X 3,317,360 5/1967 Young et al. 14922 3,122,462 2/ 1964 Kaufman et a1 149-22 BENJAMIN R. PADGETI, Primary Examiner US. Cl. X.R. 149-22, 44
US619567A 1967-03-01 1967-03-01 Ignition material containing tellurium dioxide,boron and fluoropolymeric binder Expired - Lifetime US3519505A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US61956767A 1967-03-01 1967-03-01

Publications (1)

Publication Number Publication Date
US3519505A true US3519505A (en) 1970-07-07

Family

ID=24482433

Family Applications (1)

Application Number Title Priority Date Filing Date
US619567A Expired - Lifetime US3519505A (en) 1967-03-01 1967-03-01 Ignition material containing tellurium dioxide,boron and fluoropolymeric binder

Country Status (1)

Country Link
US (1) US3519505A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3617403A (en) * 1969-04-24 1971-11-02 Duane M Johnson Ignition transfer composition comprising fuel, oxidizer and fluoroelastomer
US20100180787A1 (en) * 1996-04-26 2010-07-22 Rainer Hagel Ignition mixtures

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2410801A (en) * 1945-03-13 1946-11-12 Ludwig F Audrieth Igniting composition
US2900242A (en) * 1958-12-16 1959-08-18 Williams Harry Igniter for gas generator grains and propellants
US2953447A (en) * 1957-08-08 1960-09-20 Du Pont Ignition compositions
US2988438A (en) * 1957-04-04 1961-06-13 Olin Mathieson Combustible compositions
US3122462A (en) * 1961-11-24 1964-02-25 Martin H Kaufman Novel pyrotechnics
US3317360A (en) * 1965-03-25 1967-05-02 American Cyanamid Co Preparation of electric blasting cap mixture containing amorphous boron and lead oxide

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2410801A (en) * 1945-03-13 1946-11-12 Ludwig F Audrieth Igniting composition
US2988438A (en) * 1957-04-04 1961-06-13 Olin Mathieson Combustible compositions
US2953447A (en) * 1957-08-08 1960-09-20 Du Pont Ignition compositions
US2900242A (en) * 1958-12-16 1959-08-18 Williams Harry Igniter for gas generator grains and propellants
US3122462A (en) * 1961-11-24 1964-02-25 Martin H Kaufman Novel pyrotechnics
US3317360A (en) * 1965-03-25 1967-05-02 American Cyanamid Co Preparation of electric blasting cap mixture containing amorphous boron and lead oxide

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3617403A (en) * 1969-04-24 1971-11-02 Duane M Johnson Ignition transfer composition comprising fuel, oxidizer and fluoroelastomer
US20100180787A1 (en) * 1996-04-26 2010-07-22 Rainer Hagel Ignition mixtures
US20110162547A1 (en) * 1996-04-26 2011-07-07 Rainer Hagel Ignition mixtures

Similar Documents

Publication Publication Date Title
US8888935B2 (en) Family of modifiable high performance electrically controlled propellants and explosives
US2434652A (en) Igniter
US4144814A (en) Delay detonator device
Varesh Electric detonators: EBW and EFI
US4606272A (en) Initiation delay system for warheads with tandem mounted shaped charges
US4312271A (en) Delay detonator device
US3090310A (en) Conductive explosive primer mixture and device
WO1990013529A1 (en) Electric primer with intrinsic conductive mix
US3062143A (en) Detonator
US4994125A (en) Electric primer with intrinsic conductive mix
US5341742A (en) Firing arrangements
US4239004A (en) Delay detonator device
US3634153A (en) Noncorrosive pyrotechnic composition
US3910188A (en) One watt/one amp no-fire match type initiator
US5144893A (en) Safe ordnance initiation system
US3519505A (en) Ignition material containing tellurium dioxide,boron and fluoropolymeric binder
US3160097A (en) Molybdenum trioxide-aluminum explosive and exploding bridgewire detonator therefor
US3286628A (en) Electric detonator ignition systems
US3476623A (en) Metal azide electrically conductive priming composition and manufacture thereof
US9329011B1 (en) High voltage arm/fire device and method
US3518943A (en) Stable electrically ignitable explosive charges
US11512668B2 (en) Multi-pulse solid rocket motor ignition method
US7055434B1 (en) Electrical initiation system
US2991714A (en) Delay composition
US3182592A (en) Blasting caps