U.S. patent number 3,798,085 [Application Number 05/331,422] was granted by the patent office on 1974-03-19 for manufacture of a burning rate deterrent coated propellant.
This patent grant is currently assigned to Hercules Incorporated. Invention is credited to Dale F. Mellow.
United States Patent |
3,798,085 |
Mellow |
March 19, 1974 |
**Please see images for:
( Certificate of Correction ) ** |
MANUFACTURE OF A BURNING RATE DETERRENT COATED PROPELLANT
Abstract
Manufacture of burning rate deterrent coated propellants by
contacting a nitrocellulose smokeless powder, at an elevated
temperature, with a defined linear polyester of a new class of
burning rate deterrents, which wets, and diffuses into the
smokeless powder at the elevated temperature level, as a
plasticizer therefor, but is substantially non-migrating within the
smokeless powder at lower temperatures; effecting the contacting
step under conditions causing the polyester to coat and penetrate
the smokeless powder to form the coated propellant; and then
reducing the temperature of the resulting deterrent coated
propellant to the lower temperature above described. Also provided,
are nitrocellulose smokeless powder propellants having as a burning
rate deterrent, the defined polyester coating diffused by its own
plasticizing action into the propellant to form a resulting burning
rate gradient therefor.
Inventors: |
Mellow; Dale F. (Stanhope,
NJ) |
Assignee: |
Hercules Incorporated
(Wilmington, DE)
|
Family
ID: |
26873678 |
Appl.
No.: |
05/331,422 |
Filed: |
February 12, 1973 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
|
|
177813 |
Sep 3, 1971 |
3743554 |
|
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Current U.S.
Class: |
149/10; 149/11;
149/98 |
Current CPC
Class: |
C06B
21/0083 (20130101); C06B 45/22 (20130101) |
Current International
Class: |
C06B
45/22 (20060101); C06B 21/00 (20060101); C06B
45/00 (20060101); C06b 019/02 () |
Field of
Search: |
;149/10,11,98 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Lechert, Jr.; Stephen J.
Attorney, Agent or Firm: Stewart; S. Grant
Parent Case Text
This is a division of application Ser. No. 177,813, filed Sept. 3,
1971 now U.S. Pat. No. 3,743,554.
Claims
What I claim and desire to protect by Letters Patent is:
1. A process for the manufacture of a burning rate deterrent coated
propellant having improved burning rate gradient and ballistics
properties, which comprises contacting a nitrocellulose smokeless
powder, at an elevated temperature, with a linear polyester which
is compatible with said nitrocellulose, has a weight average
molecular weight of from about 1500 to 30,000 and a melting point
not exceeding about 190.degree.F., and which wets and diffuses into
said smokeless powder at said elevated temperature as a plasticizer
therefor but is substantially non-migrating within said smokeless
powder at lower temperatures; effecting said contacting under
conditions causing said polyester to coat, and penetrate, said
smokeless powder to form said coated propellant; and reducing the
temperature of the resulting coated propellant to a lower
temperature above described.
2. In a process of claim 1, introducing said polyester into contact
with said smokeless powder, when said polyester is dissolved in a
solvent which is a non-solvent for said nitrocellulose.
3. A process of claim 2, wherein said solvent is methylene
chloride.
4. In a process of claim 1, contacting said smokeless powder with
said polyester in the presence of water.
5. In a process of claim 2, contacting said smokeless powder with
said polyester in the presence of water, when said solvent for said
polyester is characterized by low water solubility.
6. A process of claim 4, wherein the weight ratio of said water to
said smokeless powder is within the range of from 0.05:1 to
20:1.
7. In a process of claim 1, contacting said smokeless powder with
from about 0.5 to 10 percent of its weight of said polyester, at
said elevated temperature within the range of from 150.degree. to
212.degree.F. for a period of from 1 to 200 minutes.
8. In a process of claim 7, introducing said polyester into contact
with said smokeless powder when said polyester is dissolved in a
solvent which is a non-solvent for the nitrocellulose and is
substantially water-insoluble; and contacting said smokeless powder
with said dissolved polyester, in the presence of water, in a
weight ratio of water to smokeless powder within the range of from
0.05:1 to 20:1.
9. A process of claim 8 wherein the weight average molecular weight
of said polyester is within the range of from 1500 to 20,000.
10. A process of claim 9 wherein said solvent for said polyester is
methylene chloride.
11. A process of claim 9 wherein said polyester is an ethylene
glycol-sebacic acid resin.
12. A process of claim 9 wherein said polyester is an ethylene
glycol-phthalic acid resin.
13. A process of claim 9 wherein said polyester is an ethylene
glycol-adipic acid resin.
14. A process of claim 9 wherein said polyester is a neopentyl
glycol-adipic acid resin.
15. In a process of claim 9, correlating said time, temperature,
and the amount of said polyester, for penetration of said polyester
deterrent into said smokeless powder to provide a predetermined
propellant burning rate gradient.
Description
This invention relates to improved progressive-burning smokeless
powder propellants, and to their manufacture. In one aspect this
invention relates to a process, utilizing a new class of coating
materials, as burning rate deterrents, for the manufacture of
progressive burning smokeless powder propellants having improved
burning rate gradient and ballistics properties. Other aspects will
be apparent in light of the accompanying disclosure, and the
appended claims.
It has been general practice in the propellant art to regulate
burning rate of propellants so as to produce high projectile
velocities without incurring unduly high chamber pressures, by
coating the propellant grains with a deterrent material which will
retard the initial burning rate of the grains. The practice has
been particularly applied to smokeless powder propellants. Well
known procedures for coating propellants with burning rate
deterrent materials are set forth in U.S. Pat. Nos. 2,147,698,
2,179,330, 2,198,746, and 2,187,866.
The deterrent coating materials utilized have been of two types,
based on their solubility in the propellant material, viz. the
soluble, or plasticizer type, and the insoluble, or barrier type.
The soluble, or plasticizer type, deterrent coating, due to its
ability to plasticize the propellant material penentrates the
propellant grain so that as the powder burns, the successively
exposed surfaces contain gradually less and less of the deterrent
material thus causing the combustion of the grain to proceed with
increased speed along a substantially uniform burning rate
gradient. However, although the plasticizer type deterrent coating
initially produces the desired burning rate gradient for requisite
progressive burning, those materials, during propellant storage,
continue to migrate throughout the propellant grain and, after a
period of time, they reach equilibrium concentration throughout the
grain, and hence fail to provide for the requisite burning rate
gradient. The barrier, or non-plasticizer type, does not penetrate
the propellant material and, although it does not migrate into the
propellant during storage, it neveretheless fails to provide the
progressivity of burning required for many applications. Various
means have been proposed for dilution of the barrier type
deterrents with materials soluble in the propellant material to
afford some degree of penetration and hence burning grade gradient,
but they have been disadvantageous in numerous applications,
particularly when applied to the manufacture of small arms
powders.
My invention is based on my discovery of a class of materials which
function as burning rate deterrents for smokeless powder
propellants, to provide broad uniform burning rate gradients
without appreciable migration of the deterrent material into the
propellant particles during storage; and hence provide propellants
having improved burning rate gradient, and ballistics,
stability.
In accordance with the invention a process is provided for the
manufacture of burning rate deterrent coated propellants having
improved burning rate gradient and ballistics properties, which
comprises contacting a nitrocellulose smokeless powder, at an
elevated temperature, with a linear polyester which is compatible
with said nitrocellulose, has a weight average molecular weight of
from about 1500 to 30,000 and a melting point not exceeding about
190.degree.F., which wets and diffuses into said smokeless powder
at said elevated temperature as a plasticizer therefor but is
substantially non-migrating within said smokeless powder at lower
temperatures; effecting said contacting under conditions causing
said polyester to coat, and penetrate, said smokeless powder to
form said coated propellant; and reducing the temperature of the
resulting coated propellant to a lower temperature above
described.
The invention further provides nitrocellulose smokeless powder
propellants having a linear polyester as a burning rate deterrent
coating and diffused by its own plasticizing action into said
propellant to form a resulting burning rate gradient therefor; said
polyester being compatible with said nitrocellulose, having a
weight average molecular weight of from 1500 to 30,000, a melting
point not exceeding 290.degree.190.degree.F., and being
substantially non-migrating within said smokeless powder at
temperatures not exceeding about 150.degree.F.
The invention, in preferred practice, is directed to smokeless
powder propellants, and their manufacture, for small arms, and
cannon, and to the deterrent treatment of smokeless powders for
caseless ammunition charges and other applications, including
cartridge actuated, and numerous other, industrial and military
propellant devices.
Exemplary linear polyester burning rate deterrent materials
utilized in practice of the invention are those formed from
dihydric alcohol components such as ethylene glycol, polyethylene
glycol, propylene glycol, polypropylene glycol and neopentyl
glycol, and dibasic acid components such as adipic acid, azelaic
acid, phthalic acid, and sebacic acid. Now preferred, are those
polyester deterrent materials having a weight average molecular
weight within the range of 1500 - 20,000 as further illustrated
herein. As a consequence of being compatible with the
nitrocellulose in the smokeless powder propellant, the polyester
deterrent plasticizes the smokeless powder particle surfaces and
remains in the substantially non-migrating state of diffusion,
without rendering the propellant surfaces sticky or otherwise
separating from the powder particles.
When referring herein to nitrocellulose smokeless powders, it is
meant single, double, and triple based smokeless powders well known
in the art such as illustrated in U.S. Pat. No. 3,235,425.
Generally, the smokeless powder-polyester deterrent contacting, or
coating, step is carried out at a temperature within the range of
150.degree. - 212.degree.F. for a period of from 1 to 200 minutes,
utilizing from 0.5 to 10 weight percent of the polyester deterrent
material, based on the weight of the uncoated smokeless powder.
The smokeless powder-polyester coating step is advantageously
carried out in the presence of water, the proportions of water
being variable over a broad range. I have found that in accordance
with procedure described hereinabove utilizing water as a vehicle
in an aqueous slurry coating system such as that illustrated with
reference to Example 2, the weight ratio of water to smokeless
powder in the aqueous slurry can be in the range of from 1:1 to
20:1, more often at least as high as about 4:1. On the other hand,
a lesser proportion of water can be advantageously utilized,
generally without formation of an aqueous slurry as illustrated
with reference to Example 1. In that embodiment, a weight ratio of
water to the smokeless powder in the coating system within the
range of from about 0.05:1 to about 1:1, but more often not
exceeding about 0.2:1, is utilized. Thus, although the amount of
water utilized in these embodiments, is generally within the range
of from about 0.05:1 to 20:1, the higher proportions within that
range are applicable to aqueous slurry coating systems.
I have found that it is advantageous to introduce the polyester
deterrent material into the coating step, when dissolved in a
solvent-diluent therefor, which is not a solvent for the
nitrocellulose, to lower viscosity and thereby facilitate uniform
distribution of the plyester material throughout the mass of
smokeless powder. In those embodiments carried out in the presence
of water, the solvent-diluent for the deterrent is also
characterized by low water solubility i.e. it is substantially
water insoluble. Methylene chloride is a now preferred solvent
diluent; and other solvent diluents advantageously utilized include
benzene, diethyl ether and n-butanol. The solvent-diluent generally
has a boiling point not exceeding about 125.degree.C. and is
sufficiently volatile that it can be readily evaporated from the
coating system. In other embodiments utilizing a diluent for the
polyester to be introduced into the coating system, the deterrent
is introduced into the system as an aqueous emulsion, as an aqueous
homogenized suspension, or in the case of a non-aqueous system is
dissolved in a suitable volatile non-aqueous solvent for the
polyester, which is a non-solvent for nitrocellulose.
In accordance with one embodiment, a burning rate deterrent coated
propellant of the invention is prepared by placing dry granular
smokeless powder, to be coated, in a mixing vessel equipped with
agitation means, followed, optionally, by addition of water in an
amount up to about 40 weight percent of the dry smokeless powder.
From 0.5 to 10 weight percent of the polyester deterrent coating
material, based on the uncoated smokeless powder, is then
introduced into admixture with the smokeless powder and water if
present, and is often advantageously dissolved in a suitable
diluent-solvent, which is not a solvent for the nitrocellulose in
the smokeless powder, such as in methylene chloride in about equal
weight proportions. The mixture vessel is then closed and the
powder-polyester admixture is heated under constant agitation,
generally by tumbling action, to 150.degree. - 212.degree.F. and
maintained at that temperature for a period of from about 1 to 200
minutes.
At the end of the coating period, and with continued heating, the
vessel, when methylene chloride or other volatile solvent-diluent
for the deterrent material, and/or water is present, is opened and
agitation is resumed to permit evaporation of the water and/or
diluent, and drying of the resulting coated product until it
becomes free flowing, at which time heating is terminated for
recovery of the resulting dried coated propellant product at
ambient temperature for storage.
In accordance with another embodiment of preparation of a deterrent
coated propellant of the invention, granular smokeless powder, to
be coated, is slurried in a mix tank with water in a water:
smokeless powder weight ratio above described, more often from
about 4:1 to 20:1, and the resulting slurry is maintained under
agitation conditions while adding the deterrent coating material
thereto in an amount of from about 0.5 to 10 weight percent based
on the uncoated smokeless powder, the latter optionally dissolved
in a suitable diluent, such as methylene chloride as above
described.
The resulting water slurry of deterrent coating material and
propellant powder is then heated during continued agitation to
150.degree. - 212.degree.F. and maintained at that temperature
level for a period of from 1 to 200 minutes to accomplish the
required penetration.
At the end of the coating period the temperature of the water
slurry of coated propellant product is reduced to below the storage
temperature level, generally below 150.degree.F., and the coated
propellant product is removed from the slurry and air dried to form
free flowing coated propellant.
In accordance with conventional procedure, the dry coated
propellant product can be glazed, cleaned, and blended, when
necessary, to provide the requisite ballistics.
EXAMPLE 1
A granular double base smokeless powder having an average grain
size of 0.65 inch (diameter) .times. 0.011 inch (length) was coated
with a linear polyester having a weight average molecular weight of
about 6600, as a burning rate deterrent material of the
invention.
Another portion of the same granular smokeless powder was similarly
coated with ethyl centralite, a well known plasticizer type burning
rate deterrent for propellants, to provide a "control" propellant
for comparative purposes.
The formulation of the double base granular smokeless powder to be
coated, and the burning rate deterrent coating material utilized,
are set forth in the following summary:
Granular Smokeless Powder Component Weight Percent Polyester
"control" Nitroglycerin 20.0 Component Weight Ethyl Percent Centra-
lite Nitrocellulose 77.75 Neopentyl Glycol 49.9 Diphenylamine 0.75
Adipic Acid 34.9 Barium Nitrate 1.50 Palmitic Acid 15.0
Stearic-Oleic 0.3 Acid
In carrying out the procedure for coating the smokeless powder with
the polyester burning rate deterrent, 10 pounds of the granular
smokeless powder was placed in the barrel of a jacketed tumbler
vessel, together with about two pounds of water; and two weight
percent of the polyester deterrent material, based on the weight of
the uncoated smokeless powder, was then introduced into the
smokeless powder-water admixture, as a 50 weight percent solution
in methylene chloride as a diluent therefor. The methylene chloride
solvent is not a solvent for the nitrocellulose.
The barrel of the tumbler vessel was then closed, tumbling action
was initiated, and heating fluid was circulated through the barrel
jacket to increase the temperature of the smokeless
powder/water/polyester admixture to 200.degree.F. The tumbling was
then continued at 200.degree.F. for 90 minutes during which time
coating action was complete to provide resulting coated propellant
product. At the end of the 90 minute period, the tumbling was
terminated, the barrel was opened, and tumbling was resumed at the
coating temperature level to permit evaporation of the water and
methylene chloride to provide dry free flowing coated propellant
product. The tumbling action, and circulation of heating fluid
through the jacket, were then terminated, and the coated propellant
product was then permitted to cool to ambient temperature.
The above procedure was utilized in preparation of the granular
double base smokeless powder-ethyl centralite "control" propellant,
except that the ethyl centralite was applied without a diluent
therefor.
A series of ten of each of two separate portions of each coated
propellant product was loaded after preparation as shotgun
cartridge components, and each series of cartridges was fired, one
series of each coated propellant being fired promptly after loading
and the other after an extended storage period. Each coated
propellant (product and "control") contained 1.96 weight percent of
the deterrent material. Data summarizing the firing tests are as
follows: ##SPC1##
The above data demonstrate substantially no penetration of the
polyester deterrent material into the smokeless powder grains
during storage, as evidenced by an actual decrease of 300 psi in
average maximum chamber pressure, after storage. On the other hand,
the data demonstrate ethyl centralite, a well known plasticizer
type burning rate deterrent for propellants, to have penetrated the
smokeless powder grains during preparation, comparable to that of
the polyester deterrent, but to have seriously migrated into the
smokeless powder grains, during storage, to impair the original
burning rate gradient with a resulting increase in average maximum
chamber pressure of 3500 psi.
The data demonstrate diffusion of the polyester deterrent into the
smokeless powder grains under coating temperature conditions, but
substantially no migration at storage temperature levels, generally
150.degree.F. or less, to be thereby substantially non-migrating
during storage and provide for stable burning rate gradient and
ballistics over prolonged periods.
EXAMPLE 2
One hundred grams of a double base smokeless powder propellant,
having an average grain size of 0.038 inch (diameter) .times. 0.013
inch (length) was coated with a linear polyester burning rate
deterrent material of the invention, having a weight average
molecular weight of about 16,000. The granular smokeless powder and
burning rate deterrent material are summarized as follows:
Granular Smokeless Powder The Polyester Burning Rate Deterrent
Component Weight Percent Component Weight Percent Nitroglycerin
15.0 Ethylene Glycol 29.8 Nitrocellulose 84.15 Sebacic Acid 65.4
Diphenylamine .85 Adipic Acid 1.5 C.sub.11 -C.sub.12 Dibasic 2.0
Fatty Acids Unaccounted For 1.3
In carrying out the procedure, a suspension of the granular
smokeless powder in 670 grams of water was formed in a mixing tank,
equipped with agitation means. Two percent of the deterrent coating
material, based on the weight of the uncoated smokeless powder, was
then added to the smokeless powder/water suspension as a 50 weight
percent solution in methylene chloride, under agitation conditions.
After addition of the deterrent material to the smokeless
powder/water suspension, the suspension was heated to 85.degree. -
90.degree.C. under continued agitation, after which the agitation
was continued, and the temperature maintained at 85.degree. -
90.degree.C. for an additional period of 30 minutes. At the end of
the 30 minute period, coating of the smokeless powder grains was
complete to provide resulting burning rate deterrent propellant
product of the invention; and the coated propellant product was
then recovered from the suspension and air dried. Penetration of
the polyester deterrent material into the smokeless powder grain
provided for the required ballistic properties, and the coated
propellant product was free flowing with substantially no migration
of the deterrent over prolonged storage periods to thereby exhibit
burning rate gradient and ballistics, of improved stability.
EXAMPLE 3
The procedure of Example 1 was repeated except that preparation of
the ethyl centralite formulation was omitted, the proportion of the
polyester deterrent coating material utilized was 4.5 percent
(based on the weight of the uncoated granular smokeless powder) the
coated propellant product was fired in each instance as a component
of a rifle cartridge, and the formulation of the smokeless powder
to be coated was as follows:
GRANULAR SMOKELESS POWDER
Component Weight Percent Nitroglycerin 10 Nitrocellulose 88.25
Diphenylamine 0.75 Potassium Sulfate 1.0
The coated propellant product contained 4.3 weight percent of the
polyester deterrent. These tests are further summarized as follows:
##SPC2##
The data demonstrate an increase in average maximum chamber
pressure of only 500 psi, a one percent increase, after six week
storage period, as compared with an increase of 10,500 psi, a 24
percent increase, observed for the dibutylphthalate formulation of
Example 6; and hence the marked stability of burning rate deterrent
gradient over prolonged storage periods, provided in accordance
with the invention.
EXAMPLE 4
The procedure of Example 1 was repeated utilizing the same double
base granular smokeless powder, except that the deterrent coating
material was a polyester deterrent of the invention having a weight
average molecular weight of about 1600, and preparation of the
ethyl centralite formulation was omitted. The following summarizes
the tests: ##SPC3##
The data demonstrate the improved stability of burning rate
gradient accomplished in practice of the invention, as shown by an
increase in average chamber pressure after storage, of only 600
psi, a 5.3 percent increase.
EXAMPLE 5
The procedure of Example 1 was repeated utilizing the same double
base granular smokeless powder, except that the deterrent coating
material of the invention was a polyester having a weight average
molecular weight of about 4400, and preparation of an ethyl
centralite formulation was omitted. The summarizing data are as
follow: ##SPC4##
As in the preceding examples, the above data demonstrate an
increase in average chamber pressure of 300 psi, a 2.6 percent
increase, thus again demonstrating the stable burning rate
gradients accomplished in practice of the invention.
EXAMPLE 6
The following data illustrate smokeless powder propellants having
well known burning rate deterrent materials of the soluble, or
plasticizer type, and for comparative purposes, a burning rate
deterrent coated propellant of the invention described hereinabove
with reference to Example 3. ##SPC5##
The above demonstrate substantially constant ballistics obtained in
practice of the invention as compared with increase in average
maximum chamber pressure of from 22.7 percent (DNT) to 28.7 percent
(ethyl centralite) in the prior art compositions above.
The process embodiment of the invention utilizing an aqueous slurry
type coating step is advantageously applied to water cut smokeless
powder, inasmuch as it eliminates the need for removal of the water
and residual solvent from the smokeless powder, and air drying,
prior to the coating step. The residual solvent-wet smokeless
powder, still containing from 5 to 20 parts solvent per 100 parts
of smokeless powder, generally a mixture of ethyl alcohol and
acetone in about equal volume proportions, is directly slurried
with the water for the coating step, under which conditions the
warm water due particularly to its large volume, promptly extracts
the residual solvent from the smokeless powder to eliminate the
presence of that solvent during the coating step.
The invention provides for the active control of the penetration of
the burning rate deterrent to accomplish a stable burning rate
gradient. Thus, the diffusion of the burning rate deterrent into
the propellant, and hence its plasticizing action, provides for a
degree of plasticization which increases with increase in each of
time, temperature, and amount of coating material in the coating
system; and the penetration accomplished is preserved under storage
conditions, and until use, due to the non-migration of the burning
rate deterrent within the grains. Thus by correlating temperature,
time, and amount of the deterrent material in the coating system, a
combination of coating conditions can be readily determined for
accomplishing any predetermined degree of penetration, and for then
locking in the deterrent to secure the resulting burning rate
gradient for subsequent use.
As will be evident to those skilled in the art, various
modifications can be made or followed, in light of the foregoing
disclosure and discussion, without departing from the spirit or
scope of the disclosure or from the scope of the claims.
* * * * *