US3074830A - Combustion mixtures containing guanidine nitrate - Google Patents

Combustion mixtures containing guanidine nitrate Download PDF

Info

Publication number
US3074830A
US3074830A US481A US48160A US3074830A US 3074830 A US3074830 A US 3074830A US 481 A US481 A US 481A US 48160 A US48160 A US 48160A US 3074830 A US3074830 A US 3074830A
Authority
US
United States
Prior art keywords
guanidine nitrate
parts
gas
weight
mixtures 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
US481A
Inventor
Cecil A Rassier
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US481A priority Critical patent/US3074830A/en
Application granted granted Critical
Publication of US3074830A publication Critical patent/US3074830A/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
    • C06B23/00Compositions characterised by non-explosive or non-thermic constituents
    • C06B23/007Ballistic modifiers, burning rate catalysts, burning rate depressing agents, e.g. for gas generating
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B25/00Compositions containing a nitrated organic compound
    • C06B25/34Compositions containing a nitrated organic compound the compound being a nitrated acyclic, alicyclic or heterocyclic amine
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00Compositions or products which are defined by structure or arrangement of component of product
    • C06B45/18Compositions or products which are defined by structure or arrangement of component of product comprising a coated component
    • C06B45/30Compositions or products which are defined by structure or arrangement of component of product comprising a coated component the component base containing an inorganic explosive or an inorganic thermic component
    • C06B45/32Compositions or products which are defined by structure or arrangement of component of product comprising a coated component the component base containing an inorganic explosive or an inorganic thermic component the coating containing an organic compound
    • C06B45/34Compositions or products which are defined by structure or arrangement of component of product comprising a coated component the component base containing an inorganic explosive or an inorganic thermic component the coating containing an organic compound the compound being an organic explosive or an organic thermic component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S149/00Explosive and thermic compositions or charges
    • Y10S149/11Particle size of a component
    • Y10S149/111Nitrated organic compound
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S149/00Explosive and thermic compositions or charges
    • Y10S149/11Particle size of a component
    • Y10S149/115Organic fuel

Definitions

  • the present invention relates to composition for generating gas for the purpose, inter alia, of actuating gas pressure operated devices such for instance as the propulsion of rockets and as the gas generative source for reaction motors.
  • gas generating charges may be suitable for rocket propulsion and purposes such as blasting operations and dispersion of volatilisable materials or the like they are not wholly satisfactory for purposes where it is highly desirable that the decomposition is uniform throughout the decomposition period with no excessive local over-heating within the charge.
  • An object of the present invention is to provide a gas generating charge preferably in compacted form which burns regularly to produce throughout its burning life a substantially even gas generation and homogeneous decomposition at a substantially steady temperature.
  • the invention comprises a gas generating charge comprising mixtures preferably in granular or compacted form which include guanidine nitrate or similar amidic derivatives of carbonic acid, at least one oxidising salt, and a catalyst which serves to control and to modulise the burning.
  • fillers and/or bonding agents may be incorporated, for example kaolin or china clay or wood flour.
  • the invention has particular application for use as the fuel in reaction motors, particularly small reaction motors of the type used in toy or scale aircraft or other vehicles, Where it is desired to have an even thrust throughout the length of burning without any excessive local over-heating which would damage the relatively light gauge casing of the motor.
  • the china clay or kaolin serves not only as a filler but also as a bonding agent enabling the mixture to be compacted by pressure without the inclusion of any separate bonding agent.
  • binding agents may also be employed to give adhesion between the particles in the pellet or charge.
  • heat resisting materials in addition to clay or kaolin such for example as asbestos fibre which functions solely as a heat resisting material and not as a bonding agent.
  • the mixture is ground to a suitably small mesh size.
  • the actual grain size used in the mixture depends upon the purpose for which the gas generating charge is required and the rate of burning and consequent rate of gas production and pressure created. It has been found that preferably the oxidising salt and the catalyst should be ground to a finer size than the guanidine nitrate and the grain size chosen is largely determined by the burning rate desired, the smaller the grain size the higher the speed of burning.
  • the burning temperatures can be in the region of 1200 to 1300 C. and the fuel burns satisfactorily i.e. at a steady rate up to pressures of 100 lbs. per square inch.
  • the mixtures of the present invention can be used more particularly in the compacted form as pellets or blocks in a large variety of sizes and can be stored safely without danger of spontaneous combustion or accidental igni tion otherwise than, of course, by a proper ignition temperature.
  • the pellets may be coated with a thin film of inflammable lacquer for example nitro cellulose which facilitates their handling without crumbling or fracture and at the same time the film is burnt away when the pellet is fired.
  • the invention has particular application for use in miniature gas reaction motors because the casing of these motors are usually made of aluminium or aluminium alloy in order to save weight and the mixtures of the invention have the advantage that local overheating is avoided
  • the mixtures may be used for any other purpose where gas production and gas dissemination is required and additional agents may be added to the mixture, for example to increase the burning temperature or to give any other effect required.
  • colouring materials or dyestuffs can be added to the mixture to give off a distinctively coloured combustion gas.
  • a fuel for generating gas for operating gas pressureoperated devices consisting essentially of a mixture in compacted form of guanidine nitrate to parts by weight, potassium dichromate 35 to 50 parts by weight and sesquioxide of iron 0.5 to 2 parts by weight, the said potassium dichromate and sesquioxide of iron being present in particle size smaller than the particle size of said guanidine nitrate.
  • a fuel according to claim 1 in which a bonding agent is present selected from the group consisting of kaolin, china clay and wood flour.
  • a fuel according to claim 1 in the form of a compacted pellet in the form of a compacted pellet.

Description

3,074,830 COMBUSTION MIXTURES CONTAG GUANlDlNE NrrnATn Cecil A. Rassier, 177 West St., Erith, Kent, England No Drawing. Filed Jan. 5, 1960, Ser. No. 481 Claims. (Cl. 149-2) The present invention relates to composition for generating gas for the purpose, inter alia, of actuating gas pressure operated devices such for instance as the propulsion of rockets and as the gas generative source for reaction motors.
As generating charges are already known which on local heating are capable of maintaining non detonating decomposition these charges comprise mixtures in compacted form containing guanidine nitrate and a poly-nitroor poly-nitroso-derivative of phenol or of a hydroxynitro, carboxyor methyl substitution derivatives of phenol in which the guanidine nitrate is present in propor tions predominating over the total proportions of the other constituents and the phenol derivative is present in suflicient proportion to render the compact mixture capable of sustaining its own non-detonating decomposition once initiated.
Whilst such gas generating charges may be suitable for rocket propulsion and purposes such as blasting operations and dispersion of volatilisable materials or the like they are not wholly satisfactory for purposes where it is highly desirable that the decomposition is uniform throughout the decomposition period with no excessive local over-heating within the charge.
An object of the present invention is to provide a gas generating charge preferably in compacted form which burns regularly to produce throughout its burning life a substantially even gas generation and homogeneous decomposition at a substantially steady temperature.
Broadly the invention comprises a gas generating charge comprising mixtures preferably in granular or compacted form which include guanidine nitrate or similar amidic derivatives of carbonic acid, at least one oxidising salt, and a catalyst which serves to control and to modulise the burning.
Conveniently fillers and/or bonding agents may be incorporated, for example kaolin or china clay or wood flour.
The invention has particular application for use as the fuel in reaction motors, particularly small reaction motors of the type used in toy or scale aircraft or other vehicles, Where it is desired to have an even thrust throughout the length of burning without any excessive local over-heating which would damage the relatively light gauge casing of the motor.
As an example of a suitable mix for this purpose the following is given:
80 to 90 parts guanidine nitrate 35 to 50 parts potassium dichromate .5 to 2 parts of sesquioxide of iron 1 to 3 parts kaolin or china clay All parts being by Weight The china clay or kaolin serves not only as a filler but also as a bonding agent enabling the mixture to be compacted by pressure without the inclusion of any separate bonding agent. In addition to bonding agents binding agents may also be employed to give adhesion between the particles in the pellet or charge. By varying the amount of filler the duration of burning can be controlled within certain limits.
Whilst it has been found that for the purpose stated sesquioxide of iron is at this date a preferred catalyst 3,074,830 Patented Jan. 22, 1963 which ensures substantial completion of the decomposition of the guanidine nitrate other materials may also be used for example vanadium pentoxide or other vanadate or certain compounds of molybdenum.
Furthermore there may be included into the mixtures small amounts of heat resisting materials in addition to clay or kaolin such for example as asbestos fibre which functions solely as a heat resisting material and not as a bonding agent.
In addition small quantities of a material such as potassium nitrate or potassium permanganate can be introduced up to .5 part by weight since these compounds serve to produce more complete combustion.
Conveniently the mixture is ground to a suitably small mesh size. The actual grain size used in the mixture depends upon the purpose for which the gas generating charge is required and the rate of burning and consequent rate of gas production and pressure created. It has been found that preferably the oxidising salt and the catalyst should be ground to a finer size than the guanidine nitrate and the grain size chosen is largely determined by the burning rate desired, the smaller the grain size the higher the speed of burning.
With pellets made in accordance with the present invention the burning temperatures can be in the region of 1200 to 1300 C. and the fuel burns satisfactorily i.e. at a steady rate up to pressures of 100 lbs. per square inch.
The mixtures of the present invention can be used more particularly in the compacted form as pellets or blocks in a large variety of sizes and can be stored safely without danger of spontaneous combustion or accidental igni tion otherwise than, of course, by a proper ignition temperature. Conveniently the pellets may be coated with a thin film of inflammable lacquer for example nitro cellulose which facilitates their handling without crumbling or fracture and at the same time the film is burnt away when the pellet is fired.
Whilst the invention has particular application for use in miniature gas reaction motors because the casing of these motors are usually made of aluminium or aluminium alloy in order to save weight and the mixtures of the invention have the advantage that local overheating is avoided the mixtures may be used for any other purpose where gas production and gas dissemination is required and additional agents may be added to the mixture, for example to increase the burning temperature or to give any other effect required. Thus colouring materials or dyestuffs can be added to the mixture to give off a distinctively coloured combustion gas.
What I claim is:
1. A fuel for generating gas for operating gas pressureoperated devices consisting essentially of a mixture in compacted form of guanidine nitrate to parts by weight, potassium dichromate 35 to 50 parts by weight and sesquioxide of iron 0.5 to 2 parts by weight, the said potassium dichromate and sesquioxide of iron being present in particle size smaller than the particle size of said guanidine nitrate.
2. A fuel according to claim 1 in which a bonding agent is present selected from the group consisting of kaolin, china clay and wood flour.
3. A fuel according to claim 1 in the form of a compacted pellet.
4. A fuel according to claim 1 in the form of a compacted pellet having a complete protective coating of a combustible lacquer.
5. A fuel according to claim 1 in the form of a compacted pellet having a complete protective coating of a combustible lacquer in the form of a film of nitro-cellulose lacquer.
(References on following page) References Cited in the file of this patent UNITED STATES PATENTS Taylor May 23, 1939 Hull et a1 May 20, 1952 Taylor et a1. May 5, 1953 Mace Apr. 3, 1956 OTHER REFERENCES Chemistry and Engineering News, Oct. 7, 1957, pp.
(Copy in Scientific Library.)

Claims (1)

1. A FUEL FOR GENERATING GAS FOR OPERATING GAS PRESSUREOPERATED DEVICES CONSISTING ESSENTIALLY OF A MIXTURE IN COMPACTED FORM OF GUANIDINE NITRATE 80 TO 90 PARTS BY WEIGHT, POSTASSIM DICHROMATE 35 TO 50 PARTS BY WEIGHT AND SEQUIODIDE OF IRON 0.5 TO 2 PARTS BY WEIGHT POTASSIUM DICHROMATE AND SESQUIOXIDE OF IRON BEING PRESENT IN PARTICLE SIZE SMALLER THAN THE PARTICLE SIZE OF SAID GUANIDINE NITRATE.
US481A 1960-01-05 1960-01-05 Combustion mixtures containing guanidine nitrate Expired - Lifetime US3074830A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US481A US3074830A (en) 1960-01-05 1960-01-05 Combustion mixtures containing guanidine nitrate

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US481A US3074830A (en) 1960-01-05 1960-01-05 Combustion mixtures containing guanidine nitrate

Publications (1)

Publication Number Publication Date
US3074830A true US3074830A (en) 1963-01-22

Family

ID=21691704

Family Applications (1)

Application Number Title Priority Date Filing Date
US481A Expired - Lifetime US3074830A (en) 1960-01-05 1960-01-05 Combustion mixtures containing guanidine nitrate

Country Status (1)

Country Link
US (1) US3074830A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995009825A1 (en) * 1993-10-06 1995-04-13 Nigu Chemie Gmbh Gas developing agent
DE19932466A1 (en) * 1999-07-12 2001-01-18 Trw Airbag Sys Gmbh & Co Kg Azide free gas generating composition
US20050066835A1 (en) * 2001-03-14 2005-03-31 Anders Hafstrand Propellant powder charge for barrel weapon

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2159234A (en) * 1935-03-11 1939-05-23 Ici Ltd Gas-producing nondetonating composition
US2597641A (en) * 1945-12-03 1952-05-20 Gen Electric Pressure-operated starting device
US2637274A (en) * 1946-11-29 1953-05-05 Ici Ltd Power-gas generating device
US2740702A (en) * 1945-07-27 1956-04-03 Aerojet General Co Propellant composition
US2923612A (en) * 1956-01-27 1960-02-02 Ici Ltd Gas-producing compositions
US2925942A (en) * 1957-05-21 1960-02-23 Grand Central Rocket Company Liquid dispenser

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2159234A (en) * 1935-03-11 1939-05-23 Ici Ltd Gas-producing nondetonating composition
US2740702A (en) * 1945-07-27 1956-04-03 Aerojet General Co Propellant composition
US2597641A (en) * 1945-12-03 1952-05-20 Gen Electric Pressure-operated starting device
US2637274A (en) * 1946-11-29 1953-05-05 Ici Ltd Power-gas generating device
US2923612A (en) * 1956-01-27 1960-02-02 Ici Ltd Gas-producing compositions
US2925942A (en) * 1957-05-21 1960-02-23 Grand Central Rocket Company Liquid dispenser

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995009825A1 (en) * 1993-10-06 1995-04-13 Nigu Chemie Gmbh Gas developing agent
DE19932466A1 (en) * 1999-07-12 2001-01-18 Trw Airbag Sys Gmbh & Co Kg Azide free gas generating composition
US20050066835A1 (en) * 2001-03-14 2005-03-31 Anders Hafstrand Propellant powder charge for barrel weapon

Similar Documents

Publication Publication Date Title
US2783138A (en) Propellant compositions
US3650856A (en) Red phosphorus castable smoke producing composition
US3898112A (en) Solid 5-aminotetrazole nitrate gas generating propellant with block copolymer binder
US3309249A (en) Thermite-resin binder solid fuel composition
US4130061A (en) Gun fired projectile having reduced drag
US3764420A (en) Suppression of combustion instability by means of pbi fibers
US3128706A (en) Monopropellent grains
US3074830A (en) Combustion mixtures containing guanidine nitrate
US4570540A (en) LOVA Type black powder propellant surrogate
US3473982A (en) Nitrocellulose explosive containing a charcoal binder-oxidizer mixture
US3755019A (en) Solid propellant compositions containing plasticized nitrocellulose and aluminum hydride
US3668026A (en) Castable pyrotechnic colored smoke composition
US3732130A (en) Gun propellant containing nonenergetic plasticizer,nitrocellulose and triaminoguanidine nitrate
US3946555A (en) Process for simulating turbojet engine plumes
US3017300A (en) Pelleted igniter composition and method of manufacturing same
US3044911A (en) Propellant system
US4078953A (en) Reignition suppressants for solid extinguishable propellants for use in controllable motors
US3266959A (en) Stabilized polyurethane propellants containing aluminum
US4140562A (en) Solid propellant with alginate binder
US3123507A (en) Gas-generating compositions
US3386868A (en) Heat resistant propellants containing organic oxidizers
US3383860A (en) Low flame temperature gas generant containing ammonium iodate and methode of operatin a gas generator
US3140208A (en) Gasless ignition composition for solid rocket propellants
US3873385A (en) Sodium fluoride ignition aid in solid propellant compositions
US3000718A (en) Propellant compositions