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US4452145A Expired / Lapsed US ⏱️ 0.0 years remaining

Propellant for base-bleed gas generators and process for manufacturing it

Assignee: Gechem SA
•
Filing: 1981-02-17
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Granted: 1984-06-05
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Expires: 2001-02-17
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Abstract

Abstract Process for the manufacture of a propellant for base-bleed gas generators, thus for generators made of a gas-producing charge for the increase of range wherein a binder and one or more granular or powdery solid substances are used at least one of which is an oxidant, characterized thereby that the binder is a thermoplastically deformable elastomer, that solvents are added to said elastomer which is thoroughly mixed with the solid substance and that said elastomer is deposited thereon by removal of the solvent with the formation of a granulate.

Inventors

  • 👤 Wolfgang H. R. Klohn
  • 👤 Dieter H. Muller
  • 👤 Hiltmar A. O. Schubert

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 12:41
CPC Classifications
C; C06; C06B; C06B21/00; C06B21/0008; C06B45/00; C06B45/04; C06B45/06; C06B45/10

Claims Analysis

Total Claims: 20
Claim 1
Independent Claim 70 words
A process for making a propellant for base-bleed gas generators which comprises the steps of dissolving a thermoplastically deformable elastomer in a solvent to form a solution with 10% elastomer, mixing at least one granulated oxidizer with said solution at a temperature of about 80° C., removing said solvent under vacuum by evaporation, and drying the resultant oxidizer particles coated with said elastomer at a temperature of about 50° C.
Claim 2
Dependent Claim 70 words
A process for making a propellant for base-bleed gas generators which comprises the steps of dissolving a thermoplastically deformable elastomer in a solvent to form a solution with 10% elastomer, mixing at least one granulated oxidizer with said solution at a temperature of about 80° C., removing said solvent under vacuum by evaporation, and drying the resultant oxidizer particles coated with said elastomer at a temperature of about 50° C.
Claim 3
Dependent Claim 39 words
A process according to claim 1 wherein, the obtained dried end coated particles are placed into a mold and compressed at 20 to 50 MPa under a temperature between 100° C., and 140° C., to obtain a base-bleed body.
Claim 4
Dependent Claim 17 words
A process according to claim 1, characterized in that the thermoplastically deformable elastomer is a three-block polymer.
Claim 5
Dependent Claim 28 words
A process according to claim 3, characterized in that the three-block polymer is a copolymer of butadiene and styrene or of isoprene and styrene with regular molecular arrangement.
Claim 6
Dependent Claim 15 words
A process according to claim 1, wherein said oxidizer is mixed with high-energy solid substances.
Claim 7
Dependent Claim 14 words
A process according to claim 1, wherein said oxidizer is mixed with burn-up moderators.
Claim 8
Dependent Claim 13 words
A process according to claim 1, wherein said oxidizer is mixed with plasticizers.
Claim 9
Dependent Claim 14 words
A process according to claim 1, wherein said oxidizer is mixed with a stabilizer.
Claim 10
Dependent Claim 23 words
A process according to claim 1, wherein said particles are dried until they possess a portion of volatile components of less than 0.1%.
Claim 11
Dependent Claim 22 words
A process according to claim 1, wherein said drying step is carried out in a period of time of about 12 hours.
Claim 12
Dependent Claim 86 words
A process for making a propellant for base-bleed gas generation which comprises the steps of dissolving a thermoplastically deformable elastomer in a solvent to form a solution with 10% elastomer, mixing at least one granulated oxidizer with said solution at a temperature of about 80° C., removing said solvent under vacuum by evaporation, and drying the resultant oxidizer particles coated with said elastomer at a temperature of about 50° C., said resultant oxidizer particles being suitable for use as a propellant in a base-bleed gas generator.
Claim 13
Dependent Claim 86 words
A process for making a propellant for base-bleed gas generation which comprises the steps of dissolving a thermoplastically deformable elastomer in a solvent to form a solution with 10% elastomer, mixing at least one granulated oxidizer with said solution at a temperature of about 80° C., removing said solvent under vacuum by evaporation, and drying the resultant oxidizer particles coated with said elastomer at a temperature of about 50° C., said resultant oxidizer particles being suitable for use as a propellant in a base-bleed gas generator.
Claim 14
Dependent Claim 29 words
A base bleed gas generator comprising a propellant prepared by the process according to claim 1, wherein said propellant has a burn-up speed of between 0.5 and 5.0 mm/s.
Claim 15
Dependent Claim 20 words
A base bleed gas generator according to claim 12, wherein said burn-up speed is about 1.1 to about 3.4 mm/s.
Claim 16
Dependent Claim 29 words
A base bleed gas generator according to claim 12, wherein said gas flows out at a slight overpressure of about 0.01 to about 2.00 MPa in the combustion chamber.
Claim 17
Dependent Claim 24 words
A base bleed gas generator according to claim 13, wherein said gas flows out at a pressure of about 0.11 to about 1.37 MPa.
Claim 18
Dependent Claim 19 words
A process according to claim 2, wherein said base-bleed body has a density of about 1.52 g/cm 3 .
Claim 19
Dependent Claim 75 words
A projectile comprising a base bleed gas generator to produce outcoming gases sufficient to fill the vacuum formed at the projectile bottom during flight, said vacuum otherwise causing a base drag, whereby said base drag is neutralized and the range of said projectile is increased by about 30% without active acceleration, said base bleed gas generator comprising a propellant prepared by the process according to claim 1, 3, 4, 5, 6, 7, 8 or 16.
Claim 20
Dependent Claim 65 words
A projectile comprising a base bleed gas generator to produce outcoming gases sufficient to fill the vacuum formed at the projectile bottom during flight, said vacuum otherwise causing a base drag, whereby said base drag is neutralized and the range of said projectile is increased by about 30% without active acceleration, said base bleed gas generator being one according to claim 12, 14 or 15.

References Cited (Backward Citations)

US3480488A Cited
US3539377A Cited
US3954526A Cited
US4124418A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1987-06-05 1987-12-05 1988-06-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1991-06-05 1991-12-05 1992-06-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1995-06-05 1995-12-05 1996-06-05 $7700.00 Window Closed / Lapsed

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