U.S. patent number 3,786,760 [Application Number 05/258,558] was granted by the patent office on 1974-01-22 for rotating band for projectile.
This patent grant is currently assigned to Pacific Technica Corporation. Invention is credited to Fritz K. Feldmann.
United States Patent |
3,786,760 |
Feldmann |
January 22, 1974 |
ROTATING BAND FOR PROJECTILE
Abstract
The present invention relates to the use of plastics for
rotating bands on projectiles fired from rifled gun barrels. The
plastic band is injection molded into a circumferential channel
provided in the projectile body. The cross section of the
circumferential channel is designed such as to provide a tight gas
seal between the plastic rotating band and the projectile body, to
assure transfer of spin introduced by the rifling in the gun barrel
and to secure the rotating band to the projectile after exit from
the muzzle of the gun. The portion of the plastic rotating band
protruding beyond the projectile body engraves and is compressed
into the rifling groove of the gun barrel, thus obturating the
propellant gases and transmitting the spinning motion to the
projectile. The plastic rotating band is lighter and costs less
than conventional metallic rotating bands and is, in addition, a
noncritical war material. Furthermore, its use yields better
obturation and reduced barrel wear than is obtained with
conventional rotating bands.
Inventors: |
Feldmann; Fritz K. (Santa
Barbara, CA) |
Assignee: |
Pacific Technica Corporation
(Santa Barbara, CA)
|
Family
ID: |
22981097 |
Appl.
No.: |
05/258,558 |
Filed: |
June 1, 1972 |
Current U.S.
Class: |
102/527 |
Current CPC
Class: |
F42B
14/02 (20130101) |
Current International
Class: |
F42B
14/02 (20060101); F42B 14/00 (20060101); F42b
031/00 () |
Field of
Search: |
;102/93,94,56 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Stahl; Robert F.
Claims
What is claimed is:
1. A projectile, a groove extending circumferentially of the
exterior of the projectile, said groove being recessed below the
surface of said projectile and having a generally cylindrical
section extending circumferentially of projectile together with
generally dovetailed fore and aft shoulder portions defining the
sides of said groove, a plastic rotating band located in said
groove and extending above the groove surface beyond the diameter
of said projectile to engage gun rifling to obturate the propellant
gases and to impart spin to the projectile during launch, said
cylindrical section having a smooth aft surface covering
approximately one half of said cylindrical section, a knurled
portion located fowardly of said aft surface, and a shorter smooth
surface located forwardly of the knurled surface.
2. A projectile according to claim 1 in which said rotating band
comprises an injection molded plastic.
3. A projectile according to claim 1 in which said rotating band
comprises injection molded nylon 12.
4. A projectile according to claim 1 in which said rotating band
comprises an injection molded high density polyethylene.
5. A projectile according to claim 1 in which said rotating band
comprises an injection molded polycarbonate.
6. A projectile according to claim 1 in which said rotating band
comprises an injection moldable plastic having an elastic modulus
of not less than 1 .times. 10.sup.5 psi, a tensile strength of not
less than 5,400 psi and an IZOD impact strength (notched) of not
less than 4 pounds per inch.
7. A projectile according to claim 1 in which said rotaing band
comprises a ductile, elastic plastic having a density of 0.043
pounds per cubic inch, a modulus of elasticity of 34 .times.
10.sup.5 psi, and tensile strength of 8,500 psi.
Description
BACKGROUND OF THE INVENTION
A spin stabilized projectile develops a spin or rotational motion
about its longitudinal axis as the projectile moves through a gun
barrel. The projectile carries a rotating band which is a ring-like
member encircling the aft end of the bourrelet section of the
projectile. The band protrudes circumferentially from the
projectile body so to engage the rifling grooves of the gun barrel.
During firing of the projectile, the rotating band engraves into
the rifling grooves and imparts spin to the projectile according to
the rifling twist as the projectile advances through the gun
barrel. In order for the projectile to develop the desired spin the
rotating band must not slip in the rifling grooves as through
inadequate engraving and additionally the band must not slip with
respect to the projectile body. Either condition will result in
failure of the projectile to develop full spin. The action of the
gas pressure during launch, inertial forces and frictional forces
along the barrel wall will result in shear forces between the
rotating band and the projectile body. The strength of the rotating
band and of its attachment to the projectile body must be adequate
to withstand the shear forces and to avoid unwanted slippage.
The rotating band must also perform as an obturator and prevent
leakage of the powder gases between projectile body and barrel.
Insufficient obturation will result in decreased muzzle velocity.
Small leakages can lead to very high velocities of the escaping hot
powder gases causing erosion of the barrel walls which is a major
factor in reducing barrel life. Thus, the engraving of the rotating
band with the rifling grooves of the barrel has to be complete for
satisfactory obturation and remain that way during the entire
travel of the projectile in the gun barrel.
Upon exit of the projectile from the muzzle, the rotating band must
remain on the projectile. Disintegrating rotating bands represent a
hazard to friendly troops and in the case of aircraft mounted guns
may cause damage to aircraft components as through ingestion into
the powerplant for instance. Unsymmetric deformation of the
rotating band subsequent to muzzle exit will contribute to
projectile dispersion and trajectory deviations.
The rotating band must perform the functions described above over
the entire range of environmental military conditions, i.e.,
-65.degree.F to 135.degree.F. The use of a noncritical war material
for rotating bands is desirable.
Copper alloys and sintered iron are the conventional materials used
for the manufacture of rotating bands. For some time the
application of plastics as a rotating band material has been
investigated, the primary advantages of plastics being light
weight, low cost, and low barrel wear. So far the design and
employment of plastic rotating bands has not been fully successful
for a variety of reasons.
One approach has been to secure a plastic rotating band to a metal
projectile body by means of a bonding material such as an epoxy.
There are numerous disadvantages in bonding for this particular
application. The shear strength of a well-applied bond between a
plastic and a metal surface is on the order of 1,500 psi, depending
on the specific adhesive and the materials to be bonded. This
limited shear strength either requires a wide rotating band
configuration or the use of multiple bands in order to transmit the
shear forces acting between the rotating band and the projectile
body. The use of wide or multiple rotating bands is undesirable
since they induce an increase in aerodynamic drag of the projectile
during flight.
A further disadvantage of bonding agents is their diminishing shear
strength with time (aging resistance). In addition, experience
indicates that bonds gradually weaken with age in atmospheres of
high humidity. These characteristics limit the shelf life of the
ammunition and adversely affect its immunity to adverse
environmental conditions. These disadvantages are unacceptable for
military applications.
Last, there are no valid inspection and quality control methods to
assure the quality of a bond other than by destructive testing.
This constitutes a severe handicap, particularly considering the
high production rates in the manufacture of ammunition and the high
reliability requirements for ammunition fired from automatic
weapons.
SUMMARY OF THE INVENTION
According to the present invention, a plastic rotating band is
applied preferably by injection molding to a circumferential groove
on the main projectile body. The width of of the plastic band is
approximately 50 percent larger than that of conventional metal
bands. The present invention provides a configuration for the
circumferential groove in the projectile body. The circumferential
groove for the plastic band contains a smooth cylindrical section
at its rear portion. This section acts as the gas seal and prevents
access of the high pressure propellant gases to the interface of
the rotating band and the projectile body. Ahead of the gas seal
the circumferential groove contains a knurled section which is
required to transmit the rotational motion induced by the rifling
grooves of the gun barrel to the projectile body without slippage.
Access of high temperature and high pressure propellant gases to
the knurled section such as would occur in the absence of the gas
seal will result in an excessive deformation of the rotating band
subsequent to emergence from the gun barrel, thus causing
aerodynamic assymmetries and/or loss of the rotating band. The
shoulders of the circumferential groove in the projectile body are
dovetailed to strengthen the seat of the rotating band, thus
preventing its disengagement upon exit from the gun barrel.
A ductile plastic such as a polycarbonate resin or a plastic of
similar strength properties is used as band material. The physical
properties required are such as to permit adequate engraving of the
rotating band with the rifling grooves of the barrel without
fracturing the band, and also to provide sufficient tensile
strength to withstand the centrifugal loads imposed on the band by
the high spin rate of the projectile.
The present invention can be applied to any spin stabilized
projectile. The dimensions and detailed design depends on the
particular projectile--gun configuration and the specific plastic
material selection.
The plastic rotating band can be applied to projectiles
manufactured of different metals, plastics, etc.
OBJECTS OF THE INVENTION
It is an object of the present invention to provide a plastic
rotating band which can be applied to any spin stabilized
projectile fired from a rifle gun barrel. Another object is to
provide for a plastic rotating band which can be fabricated from
low cost, non-war critical materials, using efficient production
methods. A further object of the present invention is to provide a
low weight rotating band permitting an increase in payload or an
increase in muzzle velocity of the projectile. A further object is
to provide a rotating band having improved ductility and elasticity
to yield superior propellant gas obturations to those obtainable
with conventional metal rotating bands resulting in higher muzzle
velocities for equal weight projectiles, propellant charges and
maximum chamber pressures. A further object is the reduction of
barrel wear through the use of plastic and thus the extention of
the useful life of gun barrels.
DESCRIPTION OF THE DRAWING
A preferred embodiment of the invention has been chosen for
purposes of illustration and description, and is shown in the
accompanying drawing, forming a part of the specification,
wherein:
FIG. 1 is a side elevation view partially in section of a
projectile having a rotating band according to the present
invention;
FIG. 2 is an enlarged view of the sectioned portion of FIG. 1;
FIG. 3 is a fragmentary plan view of a projectile showing the
circumferential groove with the rotating band removed;
FIG. 4 is a section view taken along line 4--4 of FIG. 2;
FIG. 5 is a section view showing a projectile within a gun barrel;
and
FIG. 6 is a section view taken along line 6--6 of FIG. 5 showing
the rotating band of the projectile engraved into the gun barrel
rifling.
DETAILED DESCRIPTION OF THE INVENTION
Referring to the drawing, a projectile 10 according to the present
invention includes a projectile nose or ogive section 12 and a
bourrelet section 14. A recessed groove 16 may be provided on the
bourrelet section for crimping of the cartridge case (not shown) to
the projectile for final assembly. The bourrelet section has a
recessed, circumferentially extending groove 18 for receiving a
rotating band 20. During launch, the rotating band serves as a gas
seal to prevent escape of propelling gases past the projectile in
the gun barrel 22 (FIG. 5) so that maximum propelling energy is
delivered to the projectile. In addition, the rotating band
engraves into the rifling grooves 24 of the gun barrel to impart
spin to the projectile.
According to the present invention, the circumferential groove 18
in the projectile cooperates with the rotating band to provide a
gas seal at the interface between the rotating band and the surface
of the projectile at the base 26 of the groove so to prevent the
escape of propelling gases past the interface. In addition the
circumferential groove 18 cooperates with the rotating band 20 to
transmit spin without slippage to the projectile as the projectile
moves and spins along the axis of the gun barrel.
As shown in the drawing, the groove 18 includes a generally channel
form cross section extending circumferentially of the projectile
and defining a generally cylindrical base 26 and upstanding
shoulders 28, 30. Each shoulder inclines approximately 30.degree.
measured from the vertical to define confronting dovetail shoulders
for retaining the rotating band. The cylindrical base 26 of the
groove is smooth over its aft portion 26a. Preferably the smooth
section 26a covers approximately one half the surface of the base
26. The provision of the smooth section 26a is essential in the use
of plastic as rotating band material in order to form the gas seal
at the interface between the rotating band and the projectile body.
For projectiles having calibers from 20 to 30 millimeters, the
width of the smooth cylindrical section 26a should be no less than
0.2 calibers. Ahead of the smooth portion is a knurled section 26b
followed again by a shorter smooth portion 26c. Radii 32, 34 define
the junctures of the cylindrical base portions 26a and 26c with the
dovetailed shoulders 30 and 28 respectively. The width of the
knurled section 26b is dimensioned such to assure the transmission
of spin induced by the rifling to the projectile without slippage.
Among other factors, this is a function of the rifling twist of the
weapon and the axial moment of inertia of the projectile. The
dovetailed shoulders 28 and 30 of the circumferential groove serve
to contain the rotating band 20 after assembly and also during the
flight of the projectile subsequent to emergence from the
barrel.
The cylindrical section 20a of the exterior of the rotating band
which protrudes beyond the diameter of the projectile body engages
the rifling grooves 24a of the gun barrel 22 (FIGS. 5 and 6). The
outside diameter of the cylindrical section of the rotating band is
dimensioned such as to completely fill the rifling grooves upon
emerging in the barrel, causing a compression of the band exceeding
the compressive yield strength of the plastic as shown in FIGS. 5
and 6. The configuration of the rotating band protruding beyond the
cylindrical main projectile body has a ramp 20b at its forward end
with a ramp angle of approximately 20.degree.. This ramp assures a
gradual initiation of engraving and is furthermore desirable for
aerodynamic reasons during the flight of the projectile.
The rear end 20c of the band has a shoulder angle equal to the
dovetail, i.e., approximately 30.degree.. The width of the
cylindrical section of the rotating band is approximately 1.5 times
the width of an equivalent metal rotating band for the same
projectile.
The compression of the rotating band is necessary to to
satisfactorily obturate the high pressure powder gases. The
engraving of the band takes place automatically upon firing and
initial motion of the projectile into the rifled gun barrel. To
accomplish the substantial deformation of the band during engraving
without breakage, a ductile and elastic plastic such as a
polycarbonate resin, nylon 12 or high density polyethylene, or
equivalent is required. The physical properties of some applicable
plastics are listed below:
Impact Tensile Elastic Strength Plastic Strength Modulus Izod
(notched) Poly- carbonate 9,500 psi 3.4.times.10.sup.5 psi 16 ft.
lb./in. Merlon Lexan Zelux Etc. Nylon 12 8,000 psi 2.times.10.sup.5
psi 4.2 ft. lb./in. High Density 5,400 psi 1.times.10.sup.5 psi 20
ft. lb./in. Polyethylene (high density, high molecular wt.)
The physical properties of these plastics are such that they can be
employed successfully over a temperature range from -65.degree.F to
135.degree.F.
Plastics are subject to shrinkage subsequent to injection molding.
The combination of post-molding shrinkage and surface tension
causes a withdrawal of the plastic from the sharp concave corners
26c of the knurled section, thus leaving open channels through
which high pressure gases could escape. Hence, the knurled section
26b does not in itself form an adequate gas seal. This phenomena is
unique for plastics due to their inherent molding shrinkage and
does not apply to conventional metal rotating band materials.
Therefore in using plastic as a rotating band material the knurled
section has to be backed up by a gas seal 26a. Over the smooth
cylindrical section 26a, the post-molding shrinkage of the plastic
causes a tightening of the plastic around the metal thus forming a
very effective gas seal at the interface of rotating band and
projectile. In order to prevent the withdrawal of the plastic from
the intersection formed by the cylindrical sections and the
dovetailed shoulders, the corners are suitably radiused at 32 and
34.
During flight the projectile is spinning at a rate determined by
the rifling twist of the barrel and the muzzle velocity. For a 20
millimeter gun having a rifling twist of 7.degree. and a projectile
fired at a muzzle velocity of 4,000 feet per second, for instance,
the rate of spin is 2,375 revolutions per second. The resultant
centrifugal forces acting on the plastic band induce a hoop stress
with the tendency to expand the rotating band. The dovetailed
shoulders of the circumferential groove prevent the expansion of
the band and contain it in its original position.
* * * * *