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US4576094A Expired / Lapsed US ⏱️ 0.0 years remaining

Fabrication of expandable polystyrene plastic ignition containers

Assignee: United States Department of the Army
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Filing: 1985-08-28
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Granted: 1986-03-18
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Expires: 2005-08-28
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Abstract

Abstract A method of fabrication of expandable polystyrene plastic ignition container is disclosed which yields an electric squib case and an ignitor charge case which can be easily loaded with a pyrotechnic charge and an ignitor charge respectively, and when in combination, serves as the ignitor system for a high length to diameter flight motor. The method of fabrication employs expandable polystyrene beads in a first predetermined amount of polystyrene beads which are first pre-expanded to about three times their original size. A second predetermined amount of expandable polystyrene beads are combined with the pre-expanded beads; the combined beads are added to a mold of the desired shape; and the mold is placed in a steam chamber to expand the combined beads to form either the squib case or ignitor charge case. The squib case and the ignitor charge case when mated as an ignitor system for a rocket motor each has the weight, density, and strength to remain in tact during an ignition phase but subsequently breaks up into small pieces which does not inflict damage to propellant in the rocket motor or cause plugging of nozzle when in operation.

Inventors

  • 👤 Jacqueline C. Meador

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 14:47
CPC Classifications
F; F42; F42B; F42B3/00; F42B3/10; F42B3/11; B; B29; B29C; B29C44/00; B29C44/34; B29C44/3461; B29C44/36; B29C44/38; B29C44/44; B29C44/445; B29C44/3415; B29C44/3426; B29K; B29K2025/00; B29L; B29L2031/00; B29L2031/777; B29L2031/7772

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 352 words
A method for fabrication of an expandable polystyrene plastic ignition container, said container having the weight, density, and strength requirements to function in a high length to diameter rocket flight motor and to remain intact until all parts of a contained ignitor charge is ignited and which said expandable polystyrene plastic ignition container subsequently breaks up into small pieces to that plugging of the nozzle of said rocket flight motor does not occur, said method comprising completing the method steps set forth under parts A, B, and C stages as follows: Part A, pre-expanding stage consisting of: (i) selecting a first predetermined quantity of a heat expandable polystyrene in the form of minute unexpanded beads; (ii) placing said predetermined quantity of heat expandable beads in boiling water; (iii) expanding said beads to approximately three times their original size; (iv) draining off excess water; Part B, blending stage consisting of: (i) selecting a second predetermined quantity of a heat expandable polystyrene in the form of minute beads; (ii) combining said first predetermined quantity of a heat expandable polystyrene in said pre-expanded form with said second predetermined quantity of a heat expandable polystyrene and mixing thoroughly to yield a twinned polystyrene beads blend consisting of about 4.5 parts by weight of said pre-expanded polystyrene beads and of about 10 parts by weight of said heat expandable polystyrene in the form of minute beads; and, Part C, molding and heat forming stage consisting of: (i) adding a predetermined quantity of said blend of twinned polystyrene beads into a casting mold of a predetermined shape for said ignitor casting container component; (ii) placing said mold containing said twinned polystyrene beads into a steam chamber; (iii) admitting steam to said steam chamber to pressurize to 250° F. with 15 psig steam; (iv) retaining said mold containing said twinned polystyrene beads under said pressurized steam for about three miutes; (v) removing said mold from said steam chamber; (vi) placing said mold containing said twinned polystyrene beads in an expanded stage into cold water for about one minute; and (vii) removing polystyrene plastic ignitor casing container from said mold.
Claim 2
Independent Claim 352 words
A method for fabrication of an expandable polystyrene plastic ignition container, said container having the weight, density, and strength requirements to function in a high length to diameter rocket flight motor and to remain intact until all parts of a contained ignitor charge is ignited and which said expandable polystyrene plastic ignition container subsequently breaks up into small pieces to that plugging of the nozzle of said rocket flight motor does not occur, said method comprising completing the method steps set forth under parts A, B, and C stages as follows: Part A, pre-expanding stage consisting of: (i) selecting a first predetermined quantity of a heat expandable polystyrene in the form of minute unexpanded beads; (ii) placing said predetermined quantity of heat expandable beads in boiling water; (iii) expanding said beads to approximately three times their original size; (iv) draining off excess water; Part B, blending stage consisting of: (i) selecting a second predetermined quantity of a heat expandable polystyrene in the form of minute beads; (ii) combining said first predetermined quantity of a heat expandable polystyrene in said pre-expanded form with said second predetermined quantity of a heat expandable polystyrene and mixing thoroughly to yield a twinned polystyrene beads blend consisting of about 4.5 parts by weight of said pre-expanded polystyrene beads and of about 10 parts by weight of said heat expandable polystyrene in the form of minute beads; and, Part C, molding and heat forming stage consisting of: (i) adding a predetermined quantity of said blend of twinned polystyrene beads into a casting mold of a predetermined shape for said ignitor casting container component; (ii) placing said mold containing said twinned polystyrene beads into a steam chamber; (iii) admitting steam to said steam chamber to pressurize to 250° F. with 15 psig steam; (iv) retaining said mold containing said twinned polystyrene beads under said pressurized steam for about three miutes; (v) removing said mold from said steam chamber; (vi) placing said mold containing said twinned polystyrene beads in an expanded stage into cold water for about one minute; and (vii) removing polystyrene plastic ignitor casing container from said mold.
Claim 3
Dependent Claim 57 words
The method for fabrication of an expandable polystyrene plastic ignition container as defined in claim 1 wherein said expandable polystyrene plastic ignition container is an electric squib case having a wall thickness of about 0.125 millimeters for containing a pyrotechnic charge and wherein said electric squib case has a weight in the range of about 1.5 grams.
Claim 4
Dependent Claim 58 words
The method for fabrication of an expandable polystyrene plastic ignition container as defined in claim 1 wherein said expandable polystyrene plastic ignition container is an ignitor charge case having a wall thickness of about 0.175 millimeters for containing an ignitor charge formulation and wherein said ignitor charge case has a weight in the range of about 3.2 grams.
Claim 5
Dependent Claim 163 words
An ignitor system for a high length to diameter flight rocket motor comprising an electric squib case containing a pyrotechnic charge in combination with an ignitor charge case containing an ignitor charge, said electric squib case fabricated from an expandable polystyrene plastic in the form of pre-expanded beads in a ratio of about 4.5 parts by weight to about 10 parts by weight of polystyrene beads that are processed by heating after being mixed and placed in a mold that is placed in a steam chamber and processed for a predetermined time period, cooled, removed, and subsequently loaded with a pyrotechnic charge, said electric squib case wall thickness being about 0.125 millimeters and said electric squib case weight being about 1.5 grams, said ignitor charge cases fabricated from an expandable polystyrene plastic employing a like process as defined hereinabove for said electric squib case, said ignitor charge case having a wall thickness of about 0.175 millimeters and a weight of about 3.2 grams.
Claim 6
Dependent Claim 163 words
An ignitor system for a high length to diameter flight rocket motor comprising an electric squib case containing a pyrotechnic charge in combination with an ignitor charge case containing an ignitor charge, said electric squib case fabricated from an expandable polystyrene plastic in the form of pre-expanded beads in a ratio of about 4.5 parts by weight to about 10 parts by weight of polystyrene beads that are processed by heating after being mixed and placed in a mold that is placed in a steam chamber and processed for a predetermined time period, cooled, removed, and subsequently loaded with a pyrotechnic charge, said electric squib case wall thickness being about 0.125 millimeters and said electric squib case weight being about 1.5 grams, said ignitor charge cases fabricated from an expandable polystyrene plastic employing a like process as defined hereinabove for said electric squib case, said ignitor charge case having a wall thickness of about 0.175 millimeters and a weight of about 3.2 grams.

References Cited (Backward Citations)

US4023996A Cited
US4039640A Cited
US4383468A Cited
US4416710A Cited
US4420931A Cited
US4466330A Cited
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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1989-03-17 1989-09-16 1990-03-18 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1993-03-17 1993-09-16 1994-03-18 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1997-03-17 1997-09-16 1998-03-18 $7700.00 Window Closed / Lapsed

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