TECHNICAL FIELD OF THE INVENTION
[0001] The present invention relates to firearms comprising components fabricated from dissimilar
metallic materials and, more specifically, to firearms comprising components fabricated
from metallurgically bonded multi-metallic materials and to firearms components comprising
metallurgically bonded multi-metallic materials. Methods for manufacturing such components
and firearms are also disclosed.
BACKGROUND OF THE INVENTION
[0002] Firearms such as handguns (e.g., pistols), including semi-automatic handguns, have
been in use for centuries. The M1911 pistol, for example, originated in the late 1890s
and it, in addition to several other handguns, were adopted for military service in
the early 1900s. Various types of handguns, including single and double action semi-automatic
pistols are used by military and law enforcement personnel, as well as by individuals,
throughout the world.
[0003] Many of the components of firearms experience high impact during firing and must
be constructed from materials that have high strength and corrosion-, impact- and
wear-resistant properties. These components are largely constructed from metallic
materials having high strength, as well as corrosion-, wear-and impact-resistance
properties, such as various iron-containing metallic materials, including stainless
steel materials. Other components that do not experience high impact or wear, or do
not require high strength, are sometimes constructed from aluminum or polymeric materials.
Some firearms have been fabricated using all stainless steel components, while others
are constructed from a combination of iron-containing materials, non-iron containing
materials, and polymeric materials. Firearm components are generally fabricated using
various metal stamping, machining, milling, metal forming, casting, forging, and other
techniques. Individual components may be welded to one another to form assemblies.
[0004] Because many firearm components are generally constructed, entirely or nearly entirely,
of heavy, rigid, durable materials such as various types of stainless steel and other
iron-containing materials, the overall weight of firearms is generally substantial.
It is desirable, for many applications, to reduce the overall weight of firearms without
reducing the strength, or the corrosion-, impact- and wear-resistance and reliability
of the firearms and their components.
U.S. Patent 6,711,819, for example, relates to firearms having lightweight but strong components made of
scandium containing aluminum alloys, which are composed of an aluminum alloy containing
alloying elements including, in addition to aluminum, from about 0.05% to about 00.30%
scandium with other elements such as magnesium, chromium, copper and zinc.
[0005] In other attempts to reduce weight, yet maintain the other desirable properties,
firearms have been constructed using components having different metallic compositions,
such as using a stainless steel slide component and an aluminum body. Other attempts
to reduce the weight of firearms have involved the use of wear-resistant polymeric
materials on the frame, generally in combination with an iron-containing slide component.
Some components, such as triggers, have been fabricated from lighter weight alloy
materials such as titanium-containing materials. While most firearm barrels are composed
of iron-containing materials, at least one attempt to reduce the weight of a barrel
is shown in
U.S. Patent 6,189,431, which discloses a lightweight composite gun barrel for a small caliber firearm having
a substantially metallic liner and an outer layer comprising fiber reinforced resin.
[0006] The explosion bonding phenomenon was observed during World War II when the force
of explosions was observed to metallurgically weld bomb fragments to impacted metal
objects. DuPont developed a practical explosion bonding process for bonding different
metallic materials in the early 1960s, which is described in
U.S. Patent 3,140,539.
[0007] The art of explosion bonding materials is well known. In general, explosion bonding
is a solid-state welding process that uses controlled explosive energy to force two
or more metals together at high pressures. The constituent metallic layers of the
resultant multi-layer composite system are joined by a high quality metallurgical
bond which generally forms an abrupt transition from the one metallic layer to the
other dissimilar metallic layer with virtually no degradation of the physical and
mechanical properties of the constituent metallic layers. The two most common resultant
bulk shapes of explosively bonded materials are rectangular sheet materials having
planar bond lines and cylindrical materials having cylindrical bond lines.
[0008] A wide range of metals can be explosively bonded to one another and multiple layers
of dissimilar metals bonded to one another in sequence to form multi-layer bonded
metallic substrates are not uncommon. Bonded bi- or multi-metallic substrates can
be machined and incorporated into a variety of products. Applications for such materials
include weld transitions between dissimilar metal components, precious metal conservation,
galvanic corrosion prevention, corrosion-resistant linings, bearing surfaces, and
radiation shielding. These materials are used in industries as diverse as hermetic
electronic packaging, marine shipbuilding, chemical processing, golf clubs, sputter
targets and cooking griddles.
SUMMARY OF THE INVENTION
[0009] In general, lighter weight firearms and firearms components are desirable. Many firearms
components have strength, hardness, wear-resistance, impact-resistance and/or durability
requirements, however, that lighter weight materials in general don't satisfy. For
many firearms components, high wear- and impact-resistance properties are required
at certain load or bearing points, or at interfaces with other components, while other
component areas have less rigorous material requirements. The applicant proposes using
lightweight metallic material(s), such as aluminum or an aluminum-containing material
or alloy, that is intimately and reliably bonded to a high strength, high impact-
and wear-resistant material, such as an iron-containing or titanium-containing material,
to provide a bonded multi-metallic material for use in the construction of firearms
and firearms components. The applicant discovered, unexpectedly, that metallurgically
bonded multi-metallic materials composed of metals having different properties and
comprising, for example, a generally lightweight material, such as aluminum or an
aluminum-containing metallic material, metallurgically bonded to a higher strength,
more wear- and impact-resistant metallic material, such as an iron- or titanium-containing
metallic material, are highly desirable for use in the construction of firearms and
firearms components.
[0010] The metallurgically bonded multi-metallic materials used for fabricating firearms
components of the present invention comprise at least two dissimilar metallic materials
and are generally provided as a multi-layered substrate. Metallurgically bonded multi-metallic
materials and firearms components of the present invention may comprise at least two
dissimilar metallic materials provided as at least two or more distinct metallic layers
having at least one metallurgical bond region. In general, the term "metallurgical
bond," as it is used in this specification, refers to a bond between two metals whose
interface is predominantly free of voids, oxide films and discontinuities. In many
cases, a metallurgical bond is characterized by a reaction zone between the two metals
that is of the order of several atomic layers on the surface of each metal.
[0011] At least two dissimilar metals may be bonded directly to one another, as is known
in the art, using a technique such as explosion bonding. Explosively bonded multi-metallic
materials are known in the art and are available commercially. Explosively bonded
multi-metallic substrates are generally fabricated by stacking dissimilar metallic
layers (e.g., having a flat sheet, cylindrical or another tubular form) next to one
another and using explosive charges to bond them to one another. The explosions generate
significant instantaneous pressures across the interface surfaces of the dissimilar
metals to bond them to one another. Alternatively, certain metallurgically bonded
multi-metallic materials may be provided using other techniques, such as metal cladding,
high pressure and thermal bonding techniques, roll bonding techniques, casting techniques,
or the like.
[0012] In some embodiments, at least two dissimilar metals may be bonded directly to one
another using roll-bonding or similar techniques. Additional dissimilar metal layers,
or additional metal layers having compositions similar to or the same as those they
bond to, may be provided using roll bonding, explosion bonding, and other metal joining
techniques. Some multi-metallic bonded substrates of the present invention may thus
contain multiple metal bond regions formed using different bonding techniques. In
one embodiment, multi-metallic substrate materials comprise dissimilar metal layers
metallurgically bonded to one another along a bond zone formed by roll bonding with
at least on additional layer metallurgically bonded to one of the metal layers along
a bond zone formed by a technique other than roll bonding, such as an explosive bonding
technique. In preferred embodiments, each of the bonding regions is characterized
by a reaction zone between adjacent metals (similar or dissimilar) that is of the
order of several atomic layers thick.
[0013] Bonded multi-metallic substrates used for fabricating firearms and firearms components
of the present invention are generally provided as sheet materials, cylindrical shapes
or other tubular shapes, from which rough blanks may be machined or otherwise fabricated.
Layers of constituent metallic materials may be as thin as about 0.1 cm or less, and
up to 10 cm or more thick. Metallurgical bond regions are typically planar when the
bonded multi-metallic materials are provided in a sheet or sheet-like form. The constituent
layers may have a generally uniform thickness, or they may have a nonuniform thickness.
Alternatively, the bond region may be generally tubular or cylindrical in bonded multi-metallic
materials having a tubular or cylindrical configuration.
[0014] Firearms and firearms components of the present invention are thus constructed from
bonded multi-metallic base materials comprising at least two dissimilar metallic materials
having different properties, such as weight, density, wear-resistance, impact-resistance,
durability, hardness, toughness, metallic luster, color and the like, bonded to one
another. The firearms components are generally designed and fabricated from multi-metallic
material substrates such that the metallic material having higher strength, toughness,
impact- and/or wear-resistance is positioned at load and/or bearing points, wear points,
impact points and/or interfaces with other components, while the metallic material
having a lower weight and, generally, lower impact- and wear-resistance properties,
is positioned at other component locations that have less rigorous material property
requirements.
[0015] Firearms components of the present invention may be fabricated from metallurgically
bonded multi-metallic materials including combinations of various iron-containing
metals and alloys such as steels and steel alloys identified by the American Iron
and Steel Institute designations ranging from 1000 to 7000 and including specifically
and without limitation, steel alloys 4140, 4340 and 8620, as well as stainless steels,
e.g. stainless steels identified by the American Iron and Steel Institute designations
ranging from 200 to 400 and including specifically and without limitation, stainless
steels 301, 302, 303, 303Se, 304, 304L, 309, 316, 316L, 321, 410, 416, 440A, 440B
and 440C bonded to non-iron containing metallic materials. Exemplary non-iron containing
metallic materials include, without limitation, aluminum and aluminum-containing metals
and alloys such as Aluminum Association alloys from the 1000 through 7000 series,
inclusive, and including specifically and without limitation, aluminum alloys 2024,
5086, 6061, 6062, 6063, and 7075, as well as aluminum alloys containing scandium and/or
other alloying elements, titanium and titanium-containing metals and alloys such as
SAE/ASTM Unified Numbering System alloys of the R50000 series and including, without
limitation, titanium alloys having an ASTM B 265 designation ranging from Grades 1-35,
magnesium and magnesium-containing metals and alloys such as SAE/ASTM Unified Numbering
System magnesium alloys of the M10000 series, copper-containing metals and alloys
such as SAE/ASTM Unified Numbering System copper alloys of the C20000 through the
C70000 series inclusive, and the like.
[0016] In some embodiments, firearms components of the present invention may be fabricated
from bonded multi-metallic materials including combinations of at least two different
iron-containing metals and alloys bonded to one another. Generally, the constituent
metals and/or alloys bonded to one another to form the bonded multi-metallic substrates
used in the present invention have different elemental compositions and different
physical properties but, in some embodiments, the constituent metals and/or alloys
of the multi-metallic substrates may have similar elemental compositions and/or physical
properties but different magnetic properties, appearances, colors, metallic lusters,
and the like. Constituent metals and alloys, and multi-metallic combinations forming
the bonded multi-metallic material may be chosen based on rigidity, density, cost,
corrosion-resistance, hardness, wear-resistance, impact-resistance, mechanical properties,
weight, fracture toughness, fatigue-resistance, metallic luster, color, creep-resistance,
elastic modulus, yield strength, resistance to stress, corrosion and/or cracking,
machinability, magnetic properties, anti-galling properties, and the like.
[0017] In one embodiment, for example, bonded multi-metallic materials and firearms components
of the present invention may comprise an iron-containing layer in combination with
a metallic layer having different properties, such as a titanium-containing layer,
an aluminum-containing layer, a copper-containing layer, a magnesium-containing layer,
or another metallic material having properties different from those of the iron-containing
layer. In another embodiment, firearms components of the present invention may incorporate
iron-containing surface layers providing high impact- and wear-resistance, with a
different material, such as an aluminum-containing and/or titanium-containing material
positioned as an intermediate layer, providing lighter weight or other properties
different from those of the iron-containing layer(s). Bonded multi-metallic substrates
having several distinct metallic layers composed of several distinct metallic materials
may be used. Multiple layers may have different thicknesses and the thickness of individual
layers may be constant, or may vary, over the surface area of the substrate material.
[0018] Exemplary bonded multi-metallic substrate materials include, for example: an iron-containing
metal or alloy, such as a steel alloy or stainless steel bonded to aluminum or an
aluminum-containing metal or alloy; an iron-containing metal or alloy, such as a steel
alloy or stainless steel bonded to titanium and/or a titanium-containing metal or
alloy; an iron-containing metal or alloy, such as a steel alloy or a stainless steel
bonded to magnesium or a magnesium-containing metal or alloy; titanium or a titanium-containing
metal or alloy bonded to aluminum or an aluminum-containing metal or alloy, or to
magnesium or a magnesium-containing metal or alloy; a copper-containing metal or alloy
bonded to an aluminum-containing metal or alloy; a copper-containing metal or alloy
bonded to magnesium and/or a magnesium-containing metal or alloy; a copper-containing
metal or alloy bonded to titanium and/or a titanium-containing metal or alloy; steel
or a steel-containing metal or alloy bonded to copper and/or a copper-containing metal
or alloy; and a stainless steel-containing alloy bonded to copper and/or a copper-containing
metal or alloy. Additional metallic layers comprising any of the materials listed
above may also be incorporated in the bonded multi-metallic substrate materials.
[0019] Firearms components of the present invention are generally fabricated using a multi-layer
substrate of the bonded multi-metallic material at least as thick as the final thickness
of the desired component. Component patterns are generally positioned or drawn or
imaged and oriented on bonded metallic substrate materials so that the material bond
line(s) are oriented and positioned as desired in the final component and the substrate
material is cut, machined, punched, water jetted, sawn or otherwise mechanically divided
to produce a rough component blank. Rough component blanks may then be further formed
or refined to desired specifications by machining, or using other suitable methods,
to the desired final component configuration and three dimensional conformation while
maintaining the desired orientation and position of bond line(s).
BRIEF DESCRIPTION OF THE DRAWINGS
[0020]
Fig. 1A shows a schematic perspective drawing of a bonded multi-metallic substrate
material with a pattern for forming a rough blank of a firearm frame component, and
Fig. 1B shows a schematic perspective drawing of a firearm frame component fabricated
from a bonded multi-metallic substrate of Fig. 1A machined to form a final, finished
multi-metallic frame component.
Fig. 2A shows a schematic perspective drawing of another embodiment of a bonded multi-metallic
substrate material with a pattern for forming a rough blank of a firearm frame component,
and Fig. 2B shows a schematic perspective drawing of a firearm frame component fabricated
from a bonded multi-metallic substrate of Fig. 2A machined to form a final, finished
multi-metallic frame component.
Fig. 3 shows a schematic perspective drawing of a firearm slide component of the present
invention fabricated from a bonded multi-metallic base material composed of multiple
metals bonded to one another.
Figs. 4A-4C schematically illustrate multiple embodiments of a firearm sear component
of the present invention fabricated from multi-metallic base sheet materials having
different structures and configurations.
Figs. 5A and 5B show schematic drawings of two embodiments of a firearm hammer component
of the present invention fabricated from a multi-metallic base sheet material composed
of multiple metals bonded to one another with the bond line arranged in different
locations.
DESCRIPTION OF THE INVENTION
[0021] In one embodiment, firearms components of the present invention are fabricated from
bonded multi-metallic materials provided as explosively bonded metallic materials.
The bonded multi-metallic materials may comprise multiple metallic materials having
different compositions and different properties, with an interface region and a bond
zone provided between each set of metallic layers. The constituent metallic layers
may contact one another directly in the interface region and bond zone. Alternatively,
metallic interlayers may be provided between adjoining metallic layers.
[0022] Bonded multi-metallic materials may comprise at least two metallic layers composed
of at least two different metallic materials having different properties. Bonded multi-metallic
materials are generally constructed as sheet materials, and firearms components of
the present invention may be machined or otherwise fabricated from sheet material
substrates. In some cases, bonded multi-metallic base materials may be constructed
as cylindrical base structures and firearms components are machined from the cylindrical
base structures. Non-metallic materials, including various types of rubbery materials,
plastics, thermoplastics, wood and the like may be mounted, or fastened, on an outer
surface of the bonded multi-metallic components, or within recesses or cavities of
the bonded multi-metallic components, for functional and decorative purposes.
[0023] Exemplary bonded multi-metallic materials include metallic base materials comprising
various ferrous and non-ferrous metals and alloys (e.g., stainless steels such as
AISI 300 series and/or 400 series stainless steels, titanium and titanium-containing
materials and alloys such as ASTM B265 Grades 1 through 5, copper-nickel alloys such
as Monel
™ K500, and copper-aluminum alloys such as aluminum-bronze) bonded to other metallic
materials including aluminum and aluminum-containing metals and alloys, such as AA6061
and/or AA 7075 as well as aluminum alloys containing scandium, and magnesium or magnesium-containing
materials and alloys such as AZ80A. The bonded multi-metallic material may also incorporate
metallic interlayers between the constituent metals to facilitate bonding or to provide
other desirable properties. In some embodiments, metal matrix composites and cermet
materials may be used as constituent materials forming bonded multi-metallic materials
and are considered "metallic" materials for purposes of this disclosure.
[0024] The bond zone preferably has a generally uniform physical and mechanical structure
along the interface region and preferably provides an abrupt transition from one metallic
layer to the other with no substantial degradation of the physical and mechanical
properties of either of the constituent metals. The bond zone is preferably characterized
by a metallurgical bond region that extends on the order of several atomic layers
on the surface of each metal and doesn't materially change the physical and mechanical
properties of either of the metals. Alternatively, the bond zone may include one or
more interlayer(s) comprising another constituent material that promotes bonding of
the two dissimilar metals with no substantial degradation of the physical and mechanical
properties of either of the constituent metals. Niobium- and tantalum-containing materials
are used as interlayer materials for some applications.
[0025] The thickness dimension of the constituent metallic layers forming the bonded multi-metallic
material may be generally equivalent or, in some embodiments, may be unequal. In one
embodiment, a bonded multi-metallic material may comprise a stainless steel or another
generally heavy, hard, impact- and wear-resistant material having a thickness less
than that of another, lighter weight metallic material, such as an aluminum-or titanium-
or magnesium-containing metal. In one embodiment, a heavier metallic layer has a thickness
of no more than about 50% the thickness of the lighter weight metallic layer; in some
embodiments the heavier metallic layer has a thickness of no more than about 40% the
thickness of the lighter metallic layer; in other embodiments, the heavier metallic
layer has a thickness of no more than about 25% the thickness of the lighter metallic
layer; in yet other embodiments, the heavier metallic layer has a thickness of no
more than about 10%, or no more than about 5%, the thickness of the lighter metallic
layer.
[0026] In some embodiments, the bonded multi-metallic material comprises layer of a generally
hard, impact- and wear-resistant material on either side of one or more intermediate
layer(s) having generally lighter weight properties. In this embodiment, the two opposite
surface layers may comprise the same or different materials, and may have equivalent
or different thicknesses. The lighter weight intermediate layer, likewise, may have
a thickness equivalent to that of one or both surface layers, or may have a different,
and generally larger, thickness. In some embodiments, the sum of the thicknesses of
the surface layers may be less than that of intermediate layer(s). In one embodiment,
the sum of the thicknesses of the surface metal layers is no more than about 50% the
thickness of the intermediate layer(s); in some embodiments the sum of the thicknesses
of the outer surface metal layer(s) is no more than about 40% the thickness of the
intermediate layer(s); in other embodiments, the sum of the thicknesses of the outer
surface metal layer(s) is no more than about 25% the thickness of the intermediate
layer(s); in yet other embodiments, the sum of the thicknesses of the outer surface
metal layer(s) is no more than about 10%, or no more than about 5%, the thickness
of the intermediate layer(s).
[0027] Fig. 1A shows a schematic diagram illustrating a bonded multi-metallic material substrate
with a firearm frame member pattern superimposed on the substrate. In this illustrative
embodiment, the bonded multi-metallic base material substrate 10 is composed of a
sheet comprising a first wear and impact-resistant metallic layer 12 bonded to a second,
dissimilar and lighter weight metallic layer 14 along an interface region at bond
zone 15. The bonded multi-metallic substrate material may be fabricated using explosion
bonding (or explosion welding) techniques that are known in the art, or using other
techniques that provide a solid state bond between the constituent metallic layers.
As shown in Fig. 1A, the more wear- and impact-resistant metallic layer 12 is arranged
at the upper portion of the firearm frame member where the frame member experiences
impact and movement in relation to other surfaces or components, such as the barrel
and slide. The lighter weight metallic layer 14 is arranged to form the lower portion
of the frame member and the handle or grip, which experiences less impact and movement
in relation to other components.
[0028] The heavier and more impact resistant constituent metallic material is preferably
at least thick enough to form the exposed surface of the upper portion of the frame
member that receives and interfaces with the barrel and the slide. In some embodiments,
the thickness M1 of the heavier and more impact resistant constituent metal is less
than about 3 cm; in other embodiments, thickness M1 is less than about 2 cm thick;
in still other embodiments, thickness M1 is less than about 1 cm thick. In particular
embodiments, the thickness M2 of the lighter constituent metallic material is generally
at least about 6 cm; may be at least about 8 cm thick; and, in yet other embodiments,
may be more than 10 cm, or more than 12 cm thick. The depth D of the multi-metallic
base material substrate is generally approximately equivalent to or slightly larger
than the dimensions of the final frame component.
[0029] A frame member blank may be cut, machined or otherwise separated from the substrate
according to the pattern shown schematically in Fig. 1A. The frame member blank may
then be further machined to provide the desired three dimensional configuration and
surface conformation of the finished frame member component 16, shown in an exemplary
configuration in Fig. 1B. The frame component may undergo further treatment and processing,
such as the application of other materials and surface treatments.
[0030] Figs. 2A and 2B shows schematic diagrams illustrating another embodiment of a bonded
multi-metallic material substrate and a finished firearm frame member blank constructed
from the substrate. In this illustrative embodiment, the bonded multi-metallic base
material substrate 10' is composed of a sheet comprising a first wear and impact-resistant
metallic layer 12' bonded to a second, dissimilar and lighter weight metallic layer
14A along an interface region at bond zone 15'. Bond zone 15' is preferably a metallurgical
bond zone and may be provided by roll bonding, explosive bonding, metal cladding,
high pressure and thermal bonding techniques, casting techniques, or the like.
[0031] In this embodiment, the thicker metallic layer 14' is composed of multiple metallic
layers 14A, 14B, 14C and 14D, with multiple bond regions 15A, 15B and 15C formed at
the interfaces of the neighboring metallic layers. Each of the metallic layers 14A,
14B, 14C and 14D may comprise the same or a similar metallic material; alternatively,
different layers may be composed of different metallic materials. Each bond region
15A, 15B and 15C may be provided using a metallurgical bonding technique, such as
roll bonding, explosive bonding, metal cladding, high pressure and thermal bonding
techniques, casting techniques, and the like, and each bond region 15A, 15B and 15C
is preferably a metallurgical bond zone.
[0032] In one embodiment, a wear- and impact-resistant metallic layer 12' comprising an
iron- or steel- or titanium-containing metallic material, such as a stainless steel
material, is arranged at the upper portion of the firearm frame member where the frame
member experiences impact and movement in relation to other surfaces or components,
such as the barrel and slide. A lighter weight metallic layer 14A comprising, for
example, an Aluminum- or titanium-containing metallic material, is bonded to layer
12' at bond zone 15', with the metallurgical bond region formed using a roll bonding
technique. An additional metallic layer 14B that may comprise a metallic material
that is the same as or different from the material of layer 14A, and bond zone 15A
at the interface of layers 14A and 14B, is a metallurgical bond formed using a technique
other than roll bonding, such as explosive bonding. Additional metallic layers 14C
and 14D, comprising metallic materials that are the same as or different from the
material of layers 14A, 14B, etc., incorporate bond zones 15B, 15C, etc., at layer
interfaces, which are characterized by metallurgical bonds formed using any one of
a variety of techniques, including explosive bonding techniques. This is an example
of metallic substrate materials composed of metallic layers, at least one metallic
layer comprising a material that is dissimilar from at least one other metallic layer,
wherein the bond zones are characterized by metallurgical bonds formed using at least
two different metal bonding techniques.
[0033] The heavier and more impact resistant constituent metallic material is preferably
at least thick enough to form the exposed surface of the upper portion of the frame
member that receives and interfaces with the barrel and the slide. In some embodiments,
the thickness M1' of the heavier and more impact resistant constituent metal is less
than about 3 cm; in other embodiments, thickness M1' is less than about 2 cm thick;
in still other embodiments, thickness M1' is less than about 1 cm thick. In some embodiments,
a composite metallic material composition formed by multiple metal layers, such as
14A, 14B, 14C and 14D comprises a lighter constituent metallic material and, in the
aggregate, is at least about 6 cm thick; may be at least about 8 cm thick; and, in
yet other embodiments, may be more than 10 cm, or more than 12 cm thick.
[0034] A frame member blank may be cut, machined or otherwise separated from the multi-metallic
substrate according to the pattern shown schematically in Fig. 2A. The frame member
blank may then be further machined to provide a desired three dimensional configuration
and surface conformation of the finished frame member component 16', shown in an exemplary
configuration in Fig. 2B. The frame component may undergo further treatment and processing,
such as the application of other materials and surface treatments.
[0035] The surfaces of framework member 16, 16' that experience high impact and relative
movement, shown as the upper surfaces of frame member component 16, 16' where the
framework member engages the slide, are formed by the more impact-resistant metallic
material layer 12, 12' and bond line 15, 15' is arranged below these surfaces in the
finished component. In some embodiments, the upper area of the framework member that
engages the slide comprises a steel alloy such as 4140 and/or a stainless steel alloy
such as 303 or 304L. In another embodiment, the upper area of the framework member
that engages the slide comprises a titanium-containing material or alloy, such as
a titanium alloy having an ASTM B 265 designation ranging from Grades 1 through 35.
A lighter weight and/or less impact resistant metallic material forms the lower portion
of the frame member, which experiences less impact and movement in relation to other
components. In some embodiments, the lower portion of the frame member comprises an
aluminum-containing material, such as aluminum alloy 6061 or 6062. In alternative
embodiments, the lower portion of the frame member comprises a titanium-containing
alloy having an ASTM B 265 designation ranging from Grades 1 through 35, and in some
embodiments, the lower portion of the frame member comprises titanium alloy Grade
2.
[0036] Fig. 3 illustrates an exemplary firearm slide component composed of a bonded multi-metallic
material having a different composition and configuration. In this illustration, slide
component 20 is fabricated from a bonded multi-metallic material comprising outer
(e.g., upper and lower) layers 22, 24 arranged on opposite surfaces of the bonded
multi-metallic material substrate with an intermediate layer 26 comprising a lighter
weight metallic material or a metallic material having another property different
from that of the outer layers. The outer surface layers 22, 24 may be composed of
the same or different materials. In one embodiment, for example, outer surface layers
22 and 24 comprise an iron-containing metal such as a stainless steel, and the intermediate
layer comprises a lighter weight metallic material such as aluminum, an aluminum-containing
material or alloy, titanium, a titanium-containing material or alloy, or the like.
The interface zones are shown as bond lines 23, 25, which may be provided as direct
bonds of the constituent materials, or may alternatively be provided as metallic interlayer(s).
The outer layers of heavier, more impact- and wear-resistant material are generally
less thick than the intermediate layer comprising the lighter weight metallic material,
and the outer layers are arranged to provide surfaces that experience high impact
and relative movement. Slide component 20 may first be provided as a blank from a
sheet of bonded multi-metallic material, as described above, and then machined to
provide the desired three-dimensional structure and surface conformation, as shown.
[0037] Figs. 4A-4C schematically illustrate multiple alternative embodiments of a firearm
sear component fabricated from bonded multi-metallic base components having different
structures and configurations. The sear component has wear points generally at the
distal portion 31 of the component and at the central bore 33. In the embodiment shown
in Fig. 4A, sear component 30A is fabricated from a bonded multi-metallic substrate
material comprising at least three constituent metallic materials. In this embodiment,
sections 32 and 34 are provided as different materials, each of the materials having
generally wear-and impact-resistant properties, such as two different iron-containing
metals, such as steel alloys or stainless steels. Section 36 experiences less wear
during operation of the firearm and is provided as a lightweight material, such as
an aluminum or titanium-containing metal. Bond interfaces are shown as bond lines
35, 37 and, in this embodiment, the thickness of each of the constituent metallic
layers is generally equivalent. Sear component 30A may first be provided as a blank
formed from a sheet of bonded multi-metallic material, and then may be machined to
provide the desired three-dimensional structure and surface conformation.
[0038] Figs. 4B and 4C schematically illustrate alternative embodiments of a firearm sear
component fabricated from multi-metallic substrate materials comprising at least two
constituent metallic materials. In the embodiment illustrated in Fig. 4B, sear component
30B comprises section 38 formed from a material having wear- and impact-resistant
properties, such a steel alloy or stainless steel material, with both wear points
31 and 33 being located in the sear component at a location within section 38. Section
40 experiences less wear during operation of the firearm and is provided as a lightweight
material such as an aluminum- or titanium-containing metal. The material interface
is shown as bond line 39. In this embodiment, the thickness of each of the constituent
metallic layers is unequal, with the heavier, more wear- and impact-resistant metallic
layer being thicker than the lighter weight metallic layer.
[0039] In the embodiment illustrated in Fig. 4C, sear component 30C comprises section 42
formed from a material having wear- and impact-resistant properties, such a steel
alloy or stainless steel material, and wear point 31 is located in the component at
a location within section 42. In this embodiment, section 44 may be provided as a
different steel alloy or stainless steel material, or it may be provided as a lightweight
material such as an aluminum- or titanium-containing metal, with wear point 33 being
located in the component at a location within section 44. The material interface is
shown as bond line 43. In this embodiment, the thickness of each of the constituent
metallic layers is unequal, and the lighter weight metallic layer is thicker than
the heavier, more wear- and impact-resistant metallic layer.
[0040] Figs. 5A and 5B schematically illustrate multiple embodiments of a firearm hammer
component fabricated from bonded multi-metallic materials having the same composition
but having different bond line geometries and, therefore, different weight and configuration
characteristics. The hammer component experiences a generally high impact zone in
the area indicated generally by reference numeral 51 and has wear points generally
at locations 52, 53 and 54. In the embodiment shown in Fig. 5A, hammer component 50A
is fabricated from a bonded multi-metallic substrate material comprising at least
two constituent metallic materials. In this embodiment, section 56 is formed from
a material having generally high wear- and impact-resistant properties, such as a
steel or stainless steel material. Section 58 experiences less wear and impact during
operation of the firearm and is provided as a lightweight material such as an aluminum-
or titanium-containing metal. The bond interface is shown as bond line 57. In this
embodiment, the high impact area and all of the wear points are located in section
58, formed from a wear-and impact-resistant metallic material. Hammer component 50A
may first be provided as a blank formed from a sheet of bonded multi-metallic material,
with the pattern aligned to appropriately orient the bond line in the hammer blank
and final hammer component. The blank may then be machined to provide the desired
three-dimensional structure and surface conformation.
[0041] Fig. 5B schematically illustrates an alternative embodiment of a firearm hammer component
50B fabricated from a bonded multi-metallic substrate material comprising at least
two constituent metallic materials. In the embodiment illustrated in Fig. 5B, section
60 is formed from a material having generally high wear- and impact-resistant properties,
such as a steel or stainless steel material. Section 62 experiences less wear and
impact during operation of the firearm and is provided as a lightweight material such
as an aluminum- or titanium-containing metal. The bond interface is shown as bond
line 61. In this embodiment, the high impact area and most, but not all, of the wear
points are located in section 60, formed from a wear-and impact-resistant metallic
material. Hammer component 50B may first be provided as a blank formed from a sheet
of bonded multi-metallic material, with the pattern aligned to appropriately orient
the bond line in the hammer blank and final hammer component. The blank may then be
machined to provide the desired three-dimensional structure and surface conformation.
[0042] Exemplary firearms components comprising bonded multi-metallic materials are illustrated
schematically and described in detail above. Those having skill in the art will recognize
that these specific embodiments are illustrative and that many additional and alternative
component designs may be conceived and implemented within framework of the invention
disclosed herein. Any of the constituent metallic materials described herein may be
used in any combination with other constituent metallic materials, and various firearms
components may be configured, and fabricated, using various combinations of bonded
multi-metallic materials. Additional firearms components that may be constructed using
bonded multi-metallic base materials include: stocks; handles; gas tubes; extractors;
sub-frames; receivers; barrels; bolts; blocks; doors; rollers; trunions; bushings;
gudgeons; actuators; magazine wells; stops; various links and pins; various housing
components; extractors; trigger mechanisms; safety mechanisms; firing chambers; grips;
plungers; ejectors, sights, and the like.
1. A firearm component (16; 16'; 20; 30; 50) fabricated from a metallic material, characterized in that the metallic material is composed of at least two metallic layers (12, 14; 12', 14A,
14B, 14C, 14D; 22, 24, 26; 32, 34, 36; 56, 58) having dissimilar properties and joined
to one another at a metallurgical bond region (15; 15', 15A, 15B, 15C; 23, 25; 35,
37; 57).
2. A firearm component according to claim 1, wherein the metallic material is fabricated
from an explosively bonded multi-metallic material.
3. A firearm component according to claim 1, wherein the metallic material is fabricated
from a multi-metallic material having a metallurgical bond formed by a roll bonding
technique.
4. A firearm component according to any preceding claim, wherein the metallic material
has a first impact-resistant layer (12; 12'; 22, 24; 32; 56) bonded to a second, dissimilar
and lighter weight layer (14; 14'; 26; 34; 58) along a metallurgical bond region (15;
15; 23, 25; 35; 57).
5. A firearm component according to claim 1, wherein the metallic material is composed
of at least three metallic layers 12', 14A, 14B, 14C, 14D; 22, 24, 26;32, 34, 36)
joined by at least two bond zones (15', 15A, 15B, 15C; 23, 25; 35, 37), and wherein
the at least two bond zones are constructed using different metal bonding techniques.
6. A firearm component according to claim 1, wherein the metallic material is composed
of a first impact-resistant layer (112') bonded to a second, dissimilar and lighter
weight layer (14') along a first metallurgical bond region (15'), and wherein the
second, dissimilar and lighter weight layer (14') comprises multiple layers (14A,
14B, 14C, 14D) bonded to one another along successive metallurgical bond regions (15A,
15B, 15C).
7. A firearm component according to claim 6, wherein the first metallurgical bond region
(15') is formed using a first metallurgical bonding technique, and at least one of
the successive metallurgical bond regions (15A, 15B, 15C) is formed using a second
metallurgical bonding technique different from the first technique.
8. A firearm component according to any of the preceding claims, wherein the metallic
material comprises an iron-containing metal bonded to a metal having lighter weight
properties.
9. A firearm component according to claim 8, wherein the lighter weight metal comprises
at least one of the following metals: aluminum, an aluminum alloy, titanium, a titanium
alloy, magnesium, and a magnesium alloy.
10. A firearm component according to any preceding claim, wherein the component is selected
from the following: frame or body; slide; barrel; sear; stock; handle; extractor;
sub-frame; receiver; block; door; roller; trunion; actuator; magazine well; housing
component; trigger mechanism; safety mechanism; firing chamber; grip; plunger; ejector
and sights.
11. A firearm component according to any of claims 1-9, wherein the component is a semi-automatic
pistol frame.
12. A firearm component according to any of claims 1-9, wherein the component is a semi-automatic
pistol slide.
13. A firearm comprising at least one of the components of any of claims 1-9.
14. A method of manufacturing a firearm component comprising: providing a bonded multi-metallic
substrate material; cutting the rough shape of the component from the bonded multi-metallic
substrate material; and machining the rough component shape to the desired three dimensional
configuration of the component.