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Publication numberUS3464088 A
Publication typeGrant
Publication dateSep 2, 1969
Filing dateJan 19, 1968
Priority dateJan 19, 1968
Publication numberUS 3464088 A, US 3464088A, US-A-3464088, US3464088 A, US3464088A
InventorsRichard G Guenter
Original AssigneeUs Army
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Apparatus for forming rocket propellant grains
US 3464088 A
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Description  (OCR text may contain errors)

Sept. 2, 1969 R. G. GUENTER 3,464,088

APPARATUS FOR FRMING ROCKET PROPELLANT GRAINS origial Filed July 16. 1965 nwmrokj BY? my,

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United States Patent O U.S. Cl. 18--12 1 Claim ABSTRACT OF THE DISCLOSURE An apparatus for forming a large grain propellant com prising an elongated cylindrical housing having a reduced section at one end, and outwardly expanding walls connecting the reduced section with a non-reduced section. A partition having a multiplicity of orifices is positioned traversely in the reduced section. A removable cap, having a tapered stake attached thereto, which extends through the non-reduced section, incloses the top of the non-reduced section. A disk shaped ram, which is positioned in the non-reduced section, slides loosely on the tapered stake. In operation, a consolidation ram forces the material through the orifices whereby retarding forces result in the formation of a larger grain than the starting material. The product is impaled on the integral stake of the removable cap and recovered therefrom.

This is a division of application Ser. No. 472,742, filed July 16, 1965, now U.S. Patent 3,390,210.

This invention relates to the processing of solid propellant rocket charges, and particularly to a process for manufacturing double-base charges with configurations complexity, overall size and dimensional precision previously unattainable by the conventional extrusion process.

The product of this process has various uses, but may be employed to particular advantage for purposes requiring large and complex shapes, as for example, for the propellant charge in a jet propulsion rocket motor.

Whereas solid propellant charges, of formulations designated composite and double-base, can and are made by processes termed casting, by far the greatest quantity have been produced by the solventless extrusion of double base formulation, and the majority of the installed manufacturing facilities in this country and elsewhere is of the latter type. This process comprises the mixing of the ingredients, usually in a water suspension, followed by removal of the excess water such as by centrifuging and hot air drying, then subsequent colloiding of the material on heated revolving rolls to form leathery sheets of propellant 0.1 in. thick. These sheets are convolute Wound into rolls, and in this form inserted into a press, from which the propellant is forced, under high pressure, through a forming die. This die has a diminishing crosssectional area, or approach section, followed by a length of uniform cross-section and, if the final product so requires, has one or more pins or stakes, that produce suitable perforations axially through the extruded product. Issuing from the press therefore, is a consolidated propellant strand of uniform cross-section but considerably smaller than before extrusion. The step of extrusion introduces stresses which must be relieved by high temperature annealing in order to fully stabilize the strain created. Also, the dynamic formation reflects the presence of irreducible batch to batch variation in the chemical and physical variations of ingredients', variations in all previous processing stages, and variations in the extrusion ice conditions, to a degree that the cross-section dimensions of the extruded grains vary sufficiently as to require subsequent machining to avoid excessive variation of ballistic properties among a quantity of rockets loaded with propellant charges made by the solventless extrusion process.

In the consolidation of the roll charge into a homogeneous strand, it is well understood by the industry that the individual strips comprising the roll are welded t0- gether in the approach section of die by pressure and dynamic flow, coupled with a continuing reduction in cross-sectional area in the approach section of the die. The minimum percentage reduction in cross-sectional area necessary for consolidation Varies with propellant composition and extrusion temperature, but is generally conceded to be about 300%. Thus a standard press, having a basket 16 in. in diameter, can produce as a solid strand product not large than 9 in. in diameter. Thus, the solventless extrusion process can produce only a small diameter product, only an axially symmetrical product, only a product having undesired internal stresses and a product that requires machining to eliminate variations in cross-sectional dimensions.

It is therefore, the object of this invention to eliminate the above restrictions by enlarging the die so that it cond tains the entire finished charge and accomplishing the consolidation of the charge through the combination of a multiplicity of small orifices located at the entrance to the die and a retarding force that is asserted immediately downstream of said orifices.

In the drawing:

FIGURE 1 of the drawing is a diagrammatical illustration of the apparatus employed in carrying out the process of this invention;

FIGURE 2 is an enlarged cross-section of the stake taken on the 2 2 line of FIGURE 1.

In the drawing, the press basket 10 is filled with sheets of propellant 11 which are extruded through partition 12 having a multiplicity of orifices 12a by the extrusion ram 13 which is powered through a shaft 14. The extruded material passes into a guide chamber 15 of greater diameter and/or greater cross-sectional area. The movement of the extruded material is opposed or retarded by a consolidation ram 16 which maintains a friction tight fit at the perimeter and slides loosely on a tapered stake 17 held in a centered position in the die 18 by a cap 19. The ram 16 supplies the initial retarding force necessary to push the extruded material against the expanding walls 20, so that instead of making a propellant grain smaller than the press basket as is the usual custom, is the means that permits a much larger grain to be formed in the die. This retarding force also performs the additional function of retaining the expanded material in the guide chamber long enough to relieve the strains in the material caused by extrusion. The ram 16 supplies the retarding force when starting the operation, however once the ram is moved to the end of the die 18 and removed, the retarding force is supplied by the friction in the guide chamber 15 of the solid mass of 21 against the walls 20. This friction continues to supply the retarding force necessary in succeeding operations and this force continues to perform the dual function of consolidating the extruded material so that it is possible to make a considerably larger grain than the receptacle from which the material is extruded and at the same time while performing the consolidation function retaining the expanded material a sufficient period to relieve stresses and strains built up by the extrusion. When the die 18 is filled with material, the die which contains a heating means (not shown) anneals the grain and the stake 17 is withdrawn by means of the cap 19. The stake 17 is tapered in a direction opposite to the flow of material and has longitudinal projections 22 tapered in direction opposite to the stake and tapered axially towards the center which govern the interior shape of the grain and which may be varied by changing the shape of the stake so that many geometrical configurations may be left in the interior of the grain depending upon the burning characteristics desired for any particular grain. Thereafter the cured grain may be removed from the die and the process continues without the ram 16 used in the initial operation by reason of the friction generated, by the movement of the mass 21 of the extruded material against the expanding walls 20 of the guide chamber 15, supplying the retarding force necessary to produce a better and much larger grain.

The retarding force so essential to the operation of this invention was observed in the normal operation of extruding small diameter grains and appeared to occur possibly one in a million extrusions and changes were made to prevent a recurrence of this occasional action. This observation revealed that the product occasionally touched and adhered to a nonfunctional, larger diameter metal sleeve and that the mass enlarged to lill the larger sleeve even though no back pressure was exerted. Thus, is is concluded that the powder to metal friction alone accomplishes the enlargement.

In the adaptation of this concept in actual practice, tests were found to be completely satisfactory, however, the first few inches of the product were not consolidated and had to be cut-off. Therefore, to avoid waste on the initial run, a plywood disk or ram was utilized and sized so that it was a friction t with the inside diameter of the mold and a very loose fit around the tapered stake, with a clearance of one to two inches, which further demonstrates that substantial back pressure is not required. The ram was not used after the initial extrusion, the first charge being cut free from the press basket in the area facing the ram 16 leaving a heel of consolidated extruded powder that acts as the consolidation ram for each succeeding extrusion.

One of the advantages of this process is that the pressure in the mold is extremely low and the mold need be only suiciently rigid to insure desired dimensional tolerances. Therefore equipment of nominal capital in- 4 vestment may be used to replace expensive equipment limited to a product of small diameter, for example nine to ten inches and at the same time produce a much larger more desirable product that may be axially unsymmetrical or contain other desired `geometrical configurations within the grain.

What is claimed is:

1. An apparatus for forming a large grain propellant, comprising a cylindrical press basket open at both ends containing sheets of propellant, a partition placed inside one end of the press basket containing a multiplicity of extrusion orifices, Said partition so placed as to provide a portion of the press basket of same cross-sectional area for movement of extruded material immediately after passage through said orifices, an extrusion ram in the other end of the press basket for forcing the propellant through `said orifices and the remainder of the press basket, a guide chamber with expanding walls to provide a larger cross-section than the press basket, a consolidation ram positioned within the guide chamber, and made operational by the friction of the extruded material against the expanding walls, a die of greater cross-sectional area than the press basket connected to the guide chamber, a stake tapered in a direction opposite` to the flow of material, having longitudinal projections tapered in a direction opposite to the stake, said longitudinal projections tapered radially towards the center and said stake attached to a cap for the purpose of centering the stake in the die for the production of a rocket propellant charge larger in cross-sectional area than the press basket and containing interior configurations regulated by the shape of the stake.

References Cited UNITED STATES PATENTS 551,306 12/1895 Converse et al. 18-12 2,263,183 11/1941 Martin 18-12 2,447,129 8/1948 Lorant 18-12 3,010,149 11/1961 De Makay 18-12 WILLIAM J. STEPHENSON, Primary Examiner

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US551306 *Dec 10, 1895 conyeese
US2263183 *May 24, 1938Nov 18, 1941Monsanto ChemicalsAuxiliary pressure means for extrusion devices
US2447129 *Sep 11, 1945Aug 17, 1948Hugo LorantExtrusion press
US3010149 *Dec 28, 1956Nov 28, 1961De Makay NicolasPowder-making
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US5391025 *Apr 21, 1992Feb 21, 1995Thiokol CorporationPropellant grain machining device
US5419501 *Nov 15, 1993May 30, 1995Thiokol CorporationPropellant grain cutting assembly
US5511914 *Feb 14, 1995Apr 30, 1996Thiokol CorporationPropellant grain machining device and method
US5615983 *Apr 22, 1996Apr 1, 1997Thiokol CorporationPropellant grain machining device and method
Classifications
U.S. Classification425/327
International ClassificationF02K9/24
Cooperative ClassificationF02K9/24, F05D2230/21
European ClassificationF02K9/24