US3028274A - Extrusion method for manufacturing smokeless powder - Google Patents
Extrusion method for manufacturing smokeless powder Download PDFInfo
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- US3028274A US3028274A US38945A US3894548A US3028274A US 3028274 A US3028274 A US 3028274A US 38945 A US38945 A US 38945A US 3894548 A US3894548 A US 3894548A US 3028274 A US3028274 A US 3028274A
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- grains
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- powder
- nitrocellulose
- mold
- Prior art date
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- 238000004519 manufacturing process Methods 0.000 title claims description 15
- 239000000843 powder Substances 0.000 title description 33
- 238000001125 extrusion Methods 0.000 title description 19
- 238000000034 method Methods 0.000 claims description 23
- 239000000020 Nitrocellulose Substances 0.000 claims description 18
- 229920001220 nitrocellulos Polymers 0.000 claims description 18
- 239000000203 mixture Substances 0.000 claims description 17
- 239000004014 plasticizer Substances 0.000 claims description 14
- 239000007787 solid Substances 0.000 claims description 13
- 239000003380 propellant Substances 0.000 claims description 2
- 238000005266 casting Methods 0.000 description 23
- 239000000463 material Substances 0.000 description 9
- 238000007596 consolidation process Methods 0.000 description 6
- 239000007788 liquid Substances 0.000 description 6
- 239000000314 lubricant Substances 0.000 description 6
- 239000002360 explosive Substances 0.000 description 5
- SNIOPGDIGTZGOP-UHFFFAOYSA-N Nitroglycerin Chemical compound [O-][N+](=O)OCC(O[N+]([O-])=O)CO[N+]([O-])=O SNIOPGDIGTZGOP-UHFFFAOYSA-N 0.000 description 4
- 239000000006 Nitroglycerin Substances 0.000 description 4
- 230000003750 conditioning effect Effects 0.000 description 4
- 229960003711 glyceryl trinitrate Drugs 0.000 description 4
- 239000008187 granular material Substances 0.000 description 3
- 239000004615 ingredient Substances 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 208000007101 Muscle Cramp Diseases 0.000 description 2
- 208000005392 Spasm Diseases 0.000 description 2
- UQLDLKMNUJERMK-UHFFFAOYSA-L di(octadecanoyloxy)lead Chemical compound [Pb+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O UQLDLKMNUJERMK-UHFFFAOYSA-L 0.000 description 2
- 125000001495 ethyl group Chemical group [H]C([H])([H])C([H])([H])* 0.000 description 2
- 231100001261 hazardous Toxicity 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 229920001296 polysiloxane Polymers 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- URAYPUMNDPQOKB-UHFFFAOYSA-N triacetin Chemical compound CC(=O)OCC(OC(C)=O)COC(C)=O URAYPUMNDPQOKB-UHFFFAOYSA-N 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- DYSXLQBUUOPLBB-UHFFFAOYSA-N 2,3-dinitrotoluene Chemical compound CC1=CC=CC([N+]([O-])=O)=C1[N+]([O-])=O DYSXLQBUUOPLBB-UHFFFAOYSA-N 0.000 description 1
- 229910001369 Brass Inorganic materials 0.000 description 1
- 239000004605 External Lubricant Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000009102 absorption Effects 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 229940073532 candelilla wax Drugs 0.000 description 1
- 235000013868 candelilla wax Nutrition 0.000 description 1
- 239000004204 candelilla wax Substances 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 239000007795 chemical reaction product Substances 0.000 description 1
- 239000003086 colorant Substances 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000002500 effect on skin Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 235000013773 glyceryl triacetate Nutrition 0.000 description 1
- 239000001087 glyceryl triacetate Substances 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- IUJAMGNYPWYUPM-UHFFFAOYSA-N hentriacontane Chemical compound CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC IUJAMGNYPWYUPM-UHFFFAOYSA-N 0.000 description 1
- 239000008241 heterogeneous mixture Substances 0.000 description 1
- 230000004807 localization Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- OTYBMLCTZGSZBG-UHFFFAOYSA-L potassium sulfate Chemical compound [K+].[K+].[O-]S([O-])(=O)=O OTYBMLCTZGSZBG-UHFFFAOYSA-L 0.000 description 1
- 229910052939 potassium sulfate Inorganic materials 0.000 description 1
- 235000011151 potassium sulphates Nutrition 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000002002 slurry Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 229960002622 triacetin Drugs 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B21/00—Apparatus or methods for working-up explosives, e.g. forming, cutting, drying
- C06B21/0033—Shaping the mixture
- C06B21/0075—Shaping the mixture by extrusion
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B25/00—Compositions containing a nitrated organic compound
- C06B25/18—Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition
- C06B25/24—Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition with nitroglycerine
- C06B25/26—Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition with nitroglycerine with an organic non-explosive or an organic non-thermic component
Definitions
- This invention relates to gas-producing charges and more particularly to a method for the production of gasproducing grains of small diametric cross section and of relatively large web.
- colloidingsolvent can be removed from large web smokeless powder grains only with extreme difficulty. This difliculty increases in magnitude until it becomes wholly impractical to make grains from solvent powder which have webs greater than about 0.5 inch. Therefore, grains of relatively large web have heretofore been manufactured by solventless extrusion or by a casting process.
- the conventional 'solventless extrusion method essentially comprises mixing the desired powder ingredients in a water slurry or mixing as a wetted mass, drying to the desired moisture content, rolling to a satisfactory colloided sheet by a suitable combination of rolling mills, forming a carpet roll from the rolled sheets, introducing the carpet roll into a hydraulic press and extruding therefrom a strand of desired cross section.
- a carpet roll As an alternative to forming a carpet roll,'the rolled sheet is sometimes divided into shaped pieces and these pieces introduced into the press. This process is hazardous due to possibility of fire during 'the rolling step.
- the remainder of the composition consisting of a mixture of essentially nonvolatile explosive and nonexplosive plasticizers, is introduced as a liquid into the bottom of the casting container through a manifold base assembly.
- This base assembly is so constructed that the incoming casting liquid is evenly distributed over the cross-sectional area at the base of the casting container and so that any air entrained in the casting liquid is prevented from rising into the powder granules and causing pitting and poor consolidation.
- the present invention is a process for the manufacture of grains of gas-producing material which comprises forming a cast mass of combustible, explosive, gas-producing material, curing the mass to insure complete consolidation, conditioning the mass at a suitable temperature for extrusion until its temperature is uniform throughout, charging the cast mass into an extrusion press and extruding the mass to form grains of small cross section.
- the solid cast mass is preferably formed so that its diameter is only slightly smaller than the diameter of the chamber of the extrusion press used so that a snug, sliding fit may be obtained.
- the mass may also be formed in oversize molds and then machined to the proper extrusion press dimensions. Both methods are equally operable but the latter obviously involves additional time and expense.
- Example 1 Cast powder masses were prepared by the casting process described herein with a composition as follows:
- Example 2 Cast powder masses were prepared by the casting proccs8 described herein with the following composition:
- extruded perforated cylinders were then cut to predetermined length to form grains which were of excellent quality and were tests showed that these grains gave ballistic performance similar to unextruded cast grains of the same composition and size.
- Example 3 Cast powder masses were prepared by the casting process described herein with a composition as follows:
- the extruded perforated cylinders were then cut to predetermined length to form grains which were of excellent quality and perfect consolidation. Firing tests showed that these grains gave ballistic performance similar to unof the same composition and size.
- the cast powder masses or charges to be extruded in th this invention may be cast by any process which produces homogeneous, well-consolidated grains.
- the process disclosed in the application of Gordon W. McCurdy, Serial No. 28,218, filed May 20, 1948, is preferred because of the quality of the grains produced. it is highly desirable and of utmost importance that the matrix of the cast be well consolidated free from pits formed by air bubbles in order to insure that the grains extruded therefrom are well consolidated and of satisfactory quality.
- the cast charges are preferably cured by storing them at a temperature of from about 30 C. to about 80 C. for the length of time necessary to complete their consolidation. Depending on the composition and the size of the charges produced by this casting process, suitable curing times spasms have been found to vary from as little as one to as many as six hundred hours.
- the cured cast powder masses or charges should be conditioned at a suitable temperature for extrusion prior to being charged into the press.
- the length of the conditioning time naturally depends on the size of the charge. For the 4%-inch charges produced and employed in Examples l, 2 and 3, a conditioning time of approximately 4 hours is satisfactory while with larger charges correspondingly longer conditioning times are required to obtain a uniform temperature throughout. After the charge reaches the desired temperature, it is inserted into the chamber of the extrusion press and extruded.
- the press temperature and pressure are functions of each specific composition and optimum conditions must be determined empirically. Otherwise, standard extrusion techniques may be followed.
- the molds or casting containers used to charges may be made from any suitable material to which the grain will not adhere such as aluminum, brass or steel. Removal of the cured charge from the container is facilitated if the interior of the container is coated with a thin film of lubricant, such as silicone grease, prior to the introduction of the casting powder.
- lubricant such as silicone grease
- silicone-type lubricant has been ound to have no effect on the ballistics of the grains made from the cast charges by extrusion according to this invention. Accordingly, silicone-type lubricant is preferred although other mold lubricants may be utilized providing that they do not materially affect the ballistics of the end product.
- the silicones are preferred. Generally, however, it is preferred to incorporate the extrusion lubricant in the cast charge and materials such as lead stearate or candelilla wax may be used for this purpose.
- the powder composition will comprise casting powder and casting liquid including the usual other ingredients, such as stabilizer, opaquing and/ or coloring agents, and lubricants. If it is desired, a pulverulent burning rate control material may be included. In such case, the rate control powder and casting powder must be in the form of a heterogeneous mixture in the casting container prior to introduction of the casting liquid in order to prevent undesirable localization of the rate control material within the casting or extruded grains.
- the following is a generalized formula of a composition suitable in accordance with this invention:
- plasticizers is meant either heating or explosive plasticizers and/or cooling or nonexplosive plasticizers and in either or both cases, substances which are substantially nonvolatile. Such substances should be so chosen as to satisfy the calorific requirements of the powder desired and should be compatible with nitrocellulose and other constituents of the powder as well as stable.
- the method which comprises uniformly combining combustible propellant composition comprising nitrocellulose with substantially nonvolatile plasticizer for nitrocellulose in a mold, curing the contents of the mold at subuntil a solid mass is obtained, and extruding the mass to form grains of smaller diameter than the mass.
- the method which comprises uniformly, combining granular smokeless powder comprising nitrocellulose with substantially nonvolatile plasticizer for nitrocellulose in a mold under substantially atmospheric conditions, curing the contents of the mold at substantially atmospheric pressure until a solid mass is obtained, and extruding the mass to form grains of smaller diameter than the mass.
- the method which comprises uniformly combining granular smokeless powder comprising nitrocellulose with submold under substantially atmospheric conditions, curing the contents of the mold at substantially atmospheric pressure and at a temperature of from about 30 to about 80 C. until a solid mass is obtained, and extruding the mass to form grains of smaller diameter than the mass.
- the method which comprises uniformly combining granular smokeless powder comprising nitrocellulose and nitroglycerin with substantially nonvolatile plasticizer for nitrocellulose in a mold, curing the contents of the mold at substantially atmospheric pressure until a solid mass is obtained, and extruding the mass to form grains of smaller diameter than the mass.
- the method which comprises uniformly combining granular smokeless powder comprising nitrocellulose and nitroglycerin with substantially nonvolatile plasticizer for nitrocellulose in a mold, curing the contents of the mold at substantially atmospheric pressure and at a temperature of from about 30 to about C. until a solid mass is obtained, and extruding the mass to form grains of smaller diameter than the mass.
- the method which comprises introducing granular smokeless powder comprising nitrocellulose into a mold, introducing nonvolatile plasticizer for nitrocellulose into the base of the mold until the powder grains in the mold are covered with the plasticizer, curing the contents of the mold at substantially atmospheric pressure and at a temperature of from about 30 to about 80 C. until a solid mass is obtained, heating the mass at substantially the predetermined extrusion temperature until the temperature of the mass is uniform throughout, and extruding the mass to form grains of smaller diameter than the mass.
Description
- of Gordon W. McCurdy,
short cylinders or other Delaware No Drawing. Filed July 15, 1948, Ser. No. 38,945 6 Claims. (Cl. 149-98) This invention relates to gas-producing charges and more particularly to a method for the production of gasproducing grains of small diametric cross section and of relatively large web.
It is well known that colloidingsolvent can be removed from large web smokeless powder grains only with extreme difficulty. This difliculty increases in magnitude until it becomes wholly impractical to make grains from solvent powder which have webs greater than about 0.5 inch. Therefore, grains of relatively large web have heretofore been manufactured by solventless extrusion or by a casting process.
The conventional 'solventless extrusion method essentially comprises mixing the desired powder ingredients in a water slurry or mixing as a wetted mass, drying to the desired moisture content, rolling to a satisfactory colloided sheet by a suitable combination of rolling mills, forming a carpet roll from the rolled sheets, introducing the carpet roll into a hydraulic press and extruding therefrom a strand of desired cross section. As an alternative to forming a carpet roll,'the rolled sheet is sometimes divided into shaped pieces and these pieces introduced into the press. This process is hazardous due to possibility of fire during 'the rolling step. In addition, poor consolidation in the extruded grains is often caused by the air between the rolled powder sheets and from a skin effect on these sheets brought about by surface evaporation or absorp tion of water, even though the press charge is evacuated prior to extrusion. Also, since considerable manual handling is involved, the overall process is relatively expensive. when demand for large diameter grains of varying webs increased, the solventless extrusion technique was found to be impractical and inefficient and even more hazardous because of the increased size of the press charge. Extrusion of large grains was also undesirable because of the increased cost and size of the necessarily larger presses.
An inherently safe and inexpensive method of fabricating homogeneously consolidated grains of large diameter has now been developed whereby grains of plastic composition, such as propellent grains of smokeless powder, may be cast utilizing inexpensive apparatus. This method and apparatus are disclosed in the copending application Serial No. 28,218, filed May 20, 1948. Essentially the casting process therein disclosed comprises initially colloiding the nitrocellulose or other high polymer with or without a portion of plasticizer and granulating it, by conventional techniques, in the form of configurations conducive to good packing. The mass of powder granules is introduced into a suitable casting container and held in place by applying pressure to the upper surface of the powder in the container. The remainder of the composition, consisting of a mixture of essentially nonvolatile explosive and nonexplosive plasticizers, is introduced as a liquid into the bottom of the casting container through a manifold base assembly. This base assembly is so constructed that the incoming casting liquid is evenly distributed over the cross-sectional area at the base of the casting container and so that any air entrained in the casting liquid is prevented from rising into the powder granules and causing pitting and poor consolidation. When the powder granules in the casting container are completely covered, the
" nited States Patent 2 casting liquid system is disconnected and the unit comprising container and base assembly is stored at a temperature and for a length of time necessary to complete curing and consolidation of the grain. The grain is then removed from the casting container.
This casting process is very satisfactory and completely adapted to the production of grains of more than 6 inches in diameter but it has been found that while grains of lesser diameter may be produced which are of equally high quality, mold and handling costs make their production expensive and ineflicient. The expense and inefiiciency increases as the size of the cast grain decreases.
It is therefore an object of this invention to provide a process for the production of grains of a combustible, explosive, gas-producing material which at the same time have a. small diametric cross section and a relatively large web.
It is a further object of this invention to provide a process for the production of such grains which is economical and relatively nonhazardous.
Generally described, the present invention is a process for the manufacture of grains of gas-producing material which comprises forming a cast mass of combustible, explosive, gas-producing material, curing the mass to insure complete consolidation, conditioning the mass at a suitable temperature for extrusion until its temperature is uniform throughout, charging the cast mass into an extrusion press and extruding the mass to form grains of small cross section. The solid cast mass is preferably formed so that its diameter is only slightly smaller than the diameter of the chamber of the extrusion press used so that a snug, sliding fit may be obtained. The mass may also be formed in oversize molds and then machined to the proper extrusion press dimensions. Both methods are equally operable but the latter obviously involves additional time and expense.
Having now described the present invention, the following examples are given for purposes of illustration.
Example 1 Cast powder masses were prepared by the casting process described herein with a composition as follows:
These masses were machined on a lathe to solid cylin-. by 12 inches long. The solid ders 4% inches in diameter cylinders were then extruded into perforated cylinders of small diameter and considerable length in a hydraulic press with conditions as follows:
Press temperature F 139-144 Powder temperature F 140 Pressure p.s.i 4400-5500 Die inside diameter "inches" 1.165 Pin diameter do 0.40
The extruded perforated cylinders were then cut to preshowed that all grains were of good quality and gave balthese extruded grains 1.20
test, in a 2 inch diameter by 12 inch extruded cast grains listic performance similar to unextruded cast grains of the same composition and size.
Example 2 Cast powder masses were prepared by the casting proccs8 described herein with the following composition:
. Percent Nitrocellulose (13.15% N) 52.3 Nitroglycerin 30.3 Ethyl centra'te 4.0 Triacctin 8.1 Dinitrotoluene 4.0 Potassium sulfate 1.3 Carbon black (add) 0.02
These masses were machined on a lathe to solid cylinders 4% inches in cylinders were then extruded into perforated cylinders of small diameter and considerable length in a hydraulic press with conditions as follows:
Press temperature; F 150-155 Powder temperature F 132-140 Pressure p.s.i.. 3200-3800 Die inside diameter inches- 1.165 Pin diameter do 0.40
The extruded perforated cylinders were then cut to predetermined length to form grains which were of excellent quality and were tests showed that these grains gave ballistic performance similar to unextruded cast grains of the same composition and size.
I Example 3 Cast powder masses were prepared by the casting process described herein with a composition as follows:
' I Percent Nitrocellulose (13.15% N) 58.5 Nitroglycerin 22.1 Ethyl ceutra 'te z 8.0 Triacetin 8.4 Diuitrotoluene 2.5 Lead stea-rate 0.5
These masses were machined on a lathe to solid cylinders 4% inches in diameter by 12 inches long. The solid cylinders were then extruded into perforated cylinders of small diameter and considerable length in a hydraulic press with conditions as follows:
Press temperature F 151-154 Powder temperature F- 140 Pressure -p.s.i 3200-4100 Die inside diameter inches 1.165 Pin diameter do 0.50
The extruded perforated cylinders were then cut to predetermined length to form grains which were of excellent quality and perfect consolidation. Firing tests showed that these grains gave ballistic performance similar to unof the same composition and size.
The cast powder masses or charges to be extruded in th this invention may be cast by any process which produces homogeneous, well-consolidated grains. The process disclosed in the application of Gordon W. McCurdy, Serial No. 28,218, filed May 20, 1948, is preferred because of the quality of the grains produced. it is highly desirable and of utmost importance that the matrix of the cast be well consolidated free from pits formed by air bubbles in order to insure that the grains extruded therefrom are well consolidated and of satisfactory quality. The cast charges are preferably cured by storing them at a temperature of from about 30 C. to about 80 C. for the length of time necessary to complete their consolidation. Depending on the composition and the size of the charges produced by this casting process, suitable curing times spasms have been found to vary from as little as one to as many as six hundred hours.
The cured cast powder masses or charges should be conditioned at a suitable temperature for extrusion prior to being charged into the press. The length of the conditioning time naturally depends on the size of the charge. For the 4%-inch charges produced and employed in Examples l, 2 and 3, a conditioning time of approximately 4 hours is satisfactory while with larger charges correspondingly longer conditioning times are required to obtain a uniform temperature throughout. After the charge reaches the desired temperature, it is inserted into the chamber of the extrusion press and extruded. The press temperature and pressure are functions of each specific composition and optimum conditions must be determined empirically. Otherwise, standard extrusion techniques may be followed.
The molds or casting containers used to charges may be made from any suitable material to which the grain will not adhere such as aluminum, brass or steel. Removal of the cured charge from the container is facilitated if the interior of the container is coated with a thin film of lubricant, such as silicone grease, prior to the introduction of the casting powder. The use of silicone-type lubricant has been ound to have no effect on the ballistics of the grains made from the cast charges by extrusion according to this invention. Accordingly, silicone-type lubricant is preferred although other mold lubricants may be utilized providing that they do not materially affect the ballistics of the end product. Moreover, where it is desired to employ an external lubricant in conjunction with the extrusion step, the silicones are preferred. Generally, however, it is preferred to incorporate the extrusion lubricant in the cast charge and materials such as lead stearate or candelilla wax may be used for this purpose.
The powder compositions which have been set forth in the examples indicate the flexibility of the process of this invention and represent preferred embodiments but are not intended to restrict its scope to those specific formu lations.
In general, the powder composition will comprise casting powder and casting liquid including the usual other ingredients, such as stabilizer, opaquing and/ or coloring agents, and lubricants. If it is desired, a pulverulent burning rate control material may be included. In such case, the rate control powder and casting powder must be in the form of a heterogeneous mixture in the casting container prior to introduction of the casting liquid in order to prevent undesirable localization of the rate control material within the casting or extruded grains. The following is a generalized formula of a composition suitable in accordance with this invention:
cast the Percent Nitrocellulose (ll.2-l3.4% N) 50-60 Plasticizers 35-47 Other ingredients (1-3.0
It will be understood that by plasticizers is meant either heating or explosive plasticizers and/or cooling or nonexplosive plasticizers and in either or both cases, substances which are substantially nonvolatile. Such substances should be so chosen as to satisfy the calorific requirements of the powder desired and should be compatible with nitrocellulose and other constituents of the powder as well as stable.
It is therefore apparent that the process of the present invention presents may advantages over prior art methods of producing large web grains of gas-producing material. Grains of combustible, explosive, gas-producing material having small diameters and relatively large webs may now be produced safely and economically. Of equal importance is the fact that grains produced by the extrusion of cast powder according to this invention are superior in quality to grains produced by the conventional stantially atmospheric pressure stantially nonvolatile plasticizer spasms solventless extrusion process and give enhanced ballistic performance.
What I claim and desire to protect by Letters Patent is:
1. In the manufacture of gas-producing charges, the method which comprises uniformly combining combustible propellant composition comprising nitrocellulose with substantially nonvolatile plasticizer for nitrocellulose in a mold, curing the contents of the mold at subuntil a solid mass is obtained, and extruding the mass to form grains of smaller diameter than the mass.
2. In the manufacture of gas-producing charges, the method which comprises uniformly, combining granular smokeless powder comprising nitrocellulose with substantially nonvolatile plasticizer for nitrocellulose in a mold under substantially atmospheric conditions, curing the contents of the mold at substantially atmospheric pressure until a solid mass is obtained, and extruding the mass to form grains of smaller diameter than the mass.
3. In the manufacture of gas-producing charges, the method which comprises uniformly combining granular smokeless powder comprising nitrocellulose with submold under substantially atmospheric conditions, curing the contents of the mold at substantially atmospheric pressure and at a temperature of from about 30 to about 80 C. until a solid mass is obtained, and extruding the mass to form grains of smaller diameter than the mass.
4. In the manufacture of gas-producing charges the method which comprises uniformly combining granular smokeless powder comprising nitrocellulose and nitroglycerin with substantially nonvolatile plasticizer for nitrocellulose in a mold, curing the contents of the mold at substantially atmospheric pressure until a solid mass is obtained, and extruding the mass to form grains of smaller diameter than the mass.
5. 1n the manufacture of gas-producing charges, the method which comprises uniformly combining granular smokeless powder comprising nitrocellulose and nitroglycerin with substantially nonvolatile plasticizer for nitrocellulose in a mold, curing the contents of the mold at substantially atmospheric pressure and at a temperature of from about 30 to about C. until a solid mass is obtained, and extruding the mass to form grains of smaller diameter than the mass.
6. In the manufacture of gas-producing charges, the method which comprises introducing granular smokeless powder comprising nitrocellulose into a mold, introducing nonvolatile plasticizer for nitrocellulose into the base of the mold until the powder grains in the mold are covered with the plasticizer, curing the contents of the mold at substantially atmospheric pressure and at a temperature of from about 30 to about 80 C. until a solid mass is obtained, heating the mass at substantially the predetermined extrusion temperature until the temperature of the mass is uniform throughout, and extruding the mass to form grains of smaller diameter than the mass.
References Cited in the file of this patent UNITED STATES PATENTS
Claims (1)
1. IN THE MANUFACTURE OF GAS-PRODUCING CHARGES, THE METHOD WHICH COMPRISES UNIFORMLY COMBINING COMBUSTIBLE PROPELLANT COMPOSITION COMPRISING NITROCELLULOSE WITH SUBSTANTIALLY NONVOLATILE PLASTICIZER FOR NITROCELLULOSE IN A MOLD, CURING THE CONTENTS OF THE MOLD AT SUBSTANTIALLY ATMOSPHERIC PRESSURE UNTIL A SOLID MASS IS OBTAINED, AND EXTRUDING THE MASS TO FORM GRAINS OF SMALLER DIAMETER THAN THE MASS.
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US38945A US3028274A (en) | 1948-07-15 | 1948-07-15 | Extrusion method for manufacturing smokeless powder |
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US38945A US3028274A (en) | 1948-07-15 | 1948-07-15 | Extrusion method for manufacturing smokeless powder |
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US3028274A true US3028274A (en) | 1962-04-03 |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3097123A (en) * | 1961-04-05 | 1963-07-09 | Beverley W Lewis | Cool, nitrocellulose base, non-carbon forming propellant |
US3185018A (en) * | 1961-08-18 | 1965-05-25 | Glenn H Damon | Method of fuel unit assembly |
US3447983A (en) * | 1967-07-31 | 1969-06-03 | Us Navy | Acetone treated nitrocellulose-based propellant and process |
US3943209A (en) * | 1964-09-21 | 1976-03-09 | The United States Of America As Represented By The Secretary Of The Army | High volumetric energy smokeless solid rocket propellant |
US4298411A (en) * | 1969-07-14 | 1981-11-03 | Hercules Incorporated | Crosslinked smokeless propellants |
US4298552A (en) * | 1968-04-29 | 1981-11-03 | Hercules Incorporated | Solventless extrusion of double base propellant prepared by a slurry process |
EP0159843A1 (en) * | 1984-04-05 | 1985-10-30 | Ireco Incorporated | Low detonation velocity explosive composition |
US4776993A (en) * | 1974-05-14 | 1988-10-11 | The United States Of America As Represented By The Secretary Of The Navy | Extrusion method for obtaining high strength composite propellants |
US4913053A (en) * | 1986-10-02 | 1990-04-03 | Western Atlas International, Inc. | Method of increasing the detonation velocity of detonating fuse |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US551306A (en) * | 1895-12-10 | conyeese | ||
US620775A (en) * | 1899-03-07 | Heinrich hoffmann | ||
US791111A (en) * | 1904-11-07 | 1905-05-30 | Alexis Felix Du Pont | Powder-die. |
US946745A (en) * | 1908-01-06 | 1910-01-18 | Schultze Gunpowder Company Ltd | Machinery or apparatus for dividing gelatinous gunpowder into particles or grains. |
US1054147A (en) * | 1911-10-03 | 1913-02-25 | Du Pont Powder Co | Cast explosive charge. |
US1510779A (en) * | 1924-10-07 | Richabd hebbmaot | ||
US1923849A (en) * | 1930-01-25 | 1933-08-22 | Ici Ltd | Propellent powder and process of manufacture |
US2320243A (en) * | 1940-03-27 | 1943-05-25 | Du Pont | Smokeless powder composition |
US2414029A (en) * | 1943-08-02 | 1947-01-07 | Carboloy Company Inc | Extrusion apparatus and process |
US2417090A (en) * | 1944-01-26 | 1947-03-11 | Olin Ind Inc | Manufacture of propellent explosives |
US2479727A (en) * | 1947-07-23 | 1949-08-23 | Daniels Farrington | Elimination of fissures with carbon dioxide |
-
1948
- 1948-07-15 US US38945A patent/US3028274A/en not_active Expired - Lifetime
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US551306A (en) * | 1895-12-10 | conyeese | ||
US620775A (en) * | 1899-03-07 | Heinrich hoffmann | ||
US1510779A (en) * | 1924-10-07 | Richabd hebbmaot | ||
US791111A (en) * | 1904-11-07 | 1905-05-30 | Alexis Felix Du Pont | Powder-die. |
US946745A (en) * | 1908-01-06 | 1910-01-18 | Schultze Gunpowder Company Ltd | Machinery or apparatus for dividing gelatinous gunpowder into particles or grains. |
US1054147A (en) * | 1911-10-03 | 1913-02-25 | Du Pont Powder Co | Cast explosive charge. |
US1923849A (en) * | 1930-01-25 | 1933-08-22 | Ici Ltd | Propellent powder and process of manufacture |
US2320243A (en) * | 1940-03-27 | 1943-05-25 | Du Pont | Smokeless powder composition |
US2414029A (en) * | 1943-08-02 | 1947-01-07 | Carboloy Company Inc | Extrusion apparatus and process |
US2417090A (en) * | 1944-01-26 | 1947-03-11 | Olin Ind Inc | Manufacture of propellent explosives |
US2479727A (en) * | 1947-07-23 | 1949-08-23 | Daniels Farrington | Elimination of fissures with carbon dioxide |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3097123A (en) * | 1961-04-05 | 1963-07-09 | Beverley W Lewis | Cool, nitrocellulose base, non-carbon forming propellant |
US3185018A (en) * | 1961-08-18 | 1965-05-25 | Glenn H Damon | Method of fuel unit assembly |
US3943209A (en) * | 1964-09-21 | 1976-03-09 | The United States Of America As Represented By The Secretary Of The Army | High volumetric energy smokeless solid rocket propellant |
US3447983A (en) * | 1967-07-31 | 1969-06-03 | Us Navy | Acetone treated nitrocellulose-based propellant and process |
US4298552A (en) * | 1968-04-29 | 1981-11-03 | Hercules Incorporated | Solventless extrusion of double base propellant prepared by a slurry process |
US4298411A (en) * | 1969-07-14 | 1981-11-03 | Hercules Incorporated | Crosslinked smokeless propellants |
US4776993A (en) * | 1974-05-14 | 1988-10-11 | The United States Of America As Represented By The Secretary Of The Navy | Extrusion method for obtaining high strength composite propellants |
EP0159843A1 (en) * | 1984-04-05 | 1985-10-30 | Ireco Incorporated | Low detonation velocity explosive composition |
US4913053A (en) * | 1986-10-02 | 1990-04-03 | Western Atlas International, Inc. | Method of increasing the detonation velocity of detonating fuse |
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