US2780019A - Gun barrel of aluminum alloy with metallic coatings - Google Patents

Gun barrel of aluminum alloy with metallic coatings Download PDF

Info

Publication number
US2780019A
US2780019A US272428A US27242852A US2780019A US 2780019 A US2780019 A US 2780019A US 272428 A US272428 A US 272428A US 27242852 A US27242852 A US 27242852A US 2780019 A US2780019 A US 2780019A
Authority
US
United States
Prior art keywords
barrel
coating
bore
aluminum alloy
plating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US272428A
Inventor
George C Sullivan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US272428A priority Critical patent/US2780019A/en
Priority to US450442A priority patent/US2990342A/en
Application granted granted Critical
Publication of US2780019A publication Critical patent/US2780019A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/02Composite barrels, i.e. barrels having multiple layers, e.g. of different materials
    • F41A21/04Barrel liners
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D11/00Electrolytic coating by surface reaction, i.e. forming conversion layers
    • C25D11/02Anodisation
    • C25D11/04Anodisation of aluminium or alloys based thereon
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/22Barrels which have undergone surface treatment, e.g. phosphating

Definitions

  • This invention relates to a firearm or more particularly to a barrel construction wherein the design and materials employed are of such a nature that the resultant product is a minimum in weight. This is accomplished in such a manner that other factors necessary in a practical and successful gun barrel, such as strength and life, are not jeopardized.
  • the present invention provides a firearm barrel made of a light-weight non-ferrous alloy, preferably aluminum, and including a bore having a plated or hard-coated in:
  • the words coated or coating are to be considered as including the words coated or plated or coating or plating.
  • the present application is a continuation-in-part of my copending application, Serial No. 215,694, filed March 15, 1951, and now abandoned.
  • the present invention also provides a method of making a firearm barrel, or the like, comprising the steps of machining the barrel from an aluminum alloy blank, drilling a bore axially of the blank, the bore having a diameter slightly in excess of the required finished diameter, and hard-coating the surface of the bore to a dimension that least that required for finished bore diameter.
  • the alloy blank itself may be originally formed in a tubular shape by the use of various well known techniques, thus. integrally containing a bore which can be finished as described hereinafter.
  • the recoil As the weight of a firearm is reduced, the recoil normally increases. While it has been found that the increase in recoil is not fatiguing to the average shooter, it may be found desirable to provide a recoil minimizing device.
  • This invention is particularly advantageous in that the decreased weight of the basic material in the barrel will allow a larger barrel cross-section which decreases barrel whip and therefore increases shooting accuracy. This larger barrel cross-section can be carried to the muzzle, thus permitting the use of a muzzle brake or blast device which can be designed into and form a part of the barrel itself. This feature permits a construction that is streamlined, pleasing to the eye in comparison to present devices, economical of manufacture and light in weight.
  • the reduced weight of the basic material used in this invention also allows for a longer barrel which is advantageous in the event of a military weapon and its accompanying bayonet.
  • a gun barrel construction in which a non-ferrous alloy is used in conjunction with a hard-plated barrel or bore; a sleeve or liner being incorporated near the chamber of the barrel if desired.
  • the preferred alloy is comprised essentially of aluminum combined with one or more group metals such as zinc, magnesium and copper,
  • group metals such as zinc, magnesium and copper
  • a material discovered to be practical and workable in this application has the following constituents: aluminum 88.5%, magnesium 2.5%, zinc 5.5%, copper 1.5%, chromium 0.30%; the remainder consisting of impurities. Obviously, these metals can be varied within reasonable limits without the resultant material being affected.
  • a preferred material of this type is a wroughtalloy which has received solution heat treatment and elevated temperature aging, and is formed by rolling or preferably by extrusion processes.
  • An alternate aluminum alloy material which may be preferred later is one in which the amount of alloying metals, notably magnesium and zinc, has been increased over that disclosed above. tensile strengths have been increased approximately 8% to date, such material being somewhat experimental in nature atthe present time.
  • a barrel of the above mentioned material will not withstand repeated firing unless a hard-plating is applied to its internal bore.
  • a typical method of chromium plating would be to insert an anode or cathode bar through the bore of the barrel and immerse the combination in an electrolyte for the plating operation; all in accordance with well-known current procedure.
  • the barrel should be anodized first and then ground to remove the oxide below the area to be plated.
  • the barrel may be desirable to give the barrel a flash of copper or nickel to seal the alloy material from water penetration causing corrosion and to prepare a better bonding surface for the chromium plate.
  • the plating is then applied by standard methods. It has been found wise to rotate the barrel during the plating operation to minimize the possibility of uneven plating thickness.
  • Efiort is made to control the thickness of the plating in order to eliminate subsequent machine operations; however, it is to be understood that the plating can be increased and later reduced to finish dimensions by polishing, grinding, reaming, honing, or the like, machine operations.
  • Another type of hard-coating has been applied to the bore with great success, such coating being applied by an electrochemical process which creates a non-metallic, hard, heat and corrosion resistant surface which is integral with the base material, not usually requiring the use of a separate plating metal, as described above.
  • One type coating can be created by passing a current through an oxidizing solution, the time of operation and intensity of current determining principally the thickness of the coating obtained, such coating being termed as surface oxidation.
  • a coating recently developed by the Glenn L. Martin Company and described in trade journals, will provide a hard, practical coating for the gun barrel of this invention; such coating having been found to be excellent.
  • a coating treatment which has resulted in a fine product consists of an electrolytic bath containing principally sulphuric acid, the temperature of which has been lowered to approximately 30 to 32 F.
  • the use of carbon dioxide as a temperature reducing medium has been found to be excellent in that the carbon dioxide not only performs a refrigerating function but enters into the reaction in such a way thatthe resultant composition of coating has extremely good resistance to wear.
  • Oxalic acid can be added to the bath solution thus permitting higher bath temperatures and resultant lowered costs of operation, but the coating may suffer some in physical characteristics.
  • the hard coating type of process distinguishable from the plating process in that the hard coating is formed from the basic material of the barrel itself instead of depositing a plating of another material on the barrel, is advantageous in that there is a surface impregnation which renders a highly efiicient joint action between the hard coating and the basic material of the barrel.
  • a dimensional growth may be associated .with the formation of the hard oxide films, and this feature should be taken into consideration inthe design of the barrel.
  • the oxide surface although extremely hard, can be finished by honing, lapping, or the like, methods to produce very smooth surfaces.
  • a gun barrel when treated according to the process above described has excellent resistance to corrosion and erosion and if designed with taper its performance can be substantially improved.
  • Figure l is a side view of a typical barrel incorporating the present invention, part of Figure 1 being shown in an enlarged and cross-sectioned manner;
  • Figure 2 is a cross-sectional view of the barrel showing details of the present invention including the provision for a sleeve or liner;
  • Figure 3 is a sectional view of the barrel showing the plating or coating applied to the bore;
  • Figure 4 is an elevational cross-sectioned view of the chamber portion of the barrel, showing an alternate liner
  • Figure 5 is a sectional view of the barrel showing said alternate liner
  • Figure 6 is a sectional view of the muzzle end of the barrel showing an integral recoil minimizing device
  • Figure 7 is a sectional view of an alternate design of barrel in which the chamber is incorporated in a liner, cooling fins provided about the chamber area, and the bore being so processed that it is provided with a tapered internal diameter;
  • Figure 8 shows a general method of hard plating the barrel and obtaining a tapered bore if desired.
  • the composite barrel of the present invention includes a barrel body 10 formed of a light-weight material such as aluminum alloy, having the usual bore 11 which may be rifled in the usual manner to provide interior helical-like lands 12. and grooves 13.
  • the barrel It is provided at its rear end with an externally threaded shank 14 or other typical means by which the barrel may be attached to the action or receiver.
  • the barrel 10, and particularly the bore 11, is coated with a hard coating 15. While it is essential in this invention to coat or plate the bore 11, it is not necessary, however, it may be desirable, to apply a coating to the outside surface of the barrel 10, such coating being accomplished in accordance with procedures outlined herein.
  • the hard coating or plating 15 may be applied to the chamber 16 to assist inpreventing erosion therein, however, I prefer to block off or mask both the chamber 16 and the threads 14 from this operation by using a vinyl tape, or the like, thus preventing interference with prior machining to close tolerances and headspacing of the barrel and action.
  • the barrel can, if desired, be substantially machine finished prior to plating or coating, leaving .001 to .004 inch or less tolerance for the thickness of the coating to be ap' plied.
  • the rear end of the barrel 10 contains the usual chamber 16, the size and shape of which is determined by the cartridge and caliber used.
  • the explosion pressures are a maximum in the area of the chamber 16 and reduce in the direction of the muzzle 17. While available lightweight metals have been found to have sufiicient strength to withstand with safety the explosion pressures encountered, it may be advisable, if a barrel of exceedingly lowweight is wanted, to incorporate a sleeve 18 around the chamber 16 area where pressures are at a maximum. An alternate sleeve or liner 19 may be incorporated adjacent the chamber 16; this type of strengthening element having the additional advantage of being removable and replaceable in event of excessive erosion due to repeated firing.
  • Both the sleeve 18 and the liner 19 may be installed by sweating the parts together or by furnace brazing, or the like.
  • the heat produced as a result of firing tends to increase joint efiiciency action and thus permit each element to absorb its proportion of the stresses produced.
  • the sleeve 18 can drop into detents 20 for security and the liner 19 can be secured by conventional means, such as threading, and the like.
  • the sleeve 18 or liner 19 is preferably made of a high-strength metal such as stainless steel, which has a tensile strength approaching 125,000 pounds per square inch, or a titanium alloy having a tensile strength in excess of 150,000 pounds per square inch; the latter having the additional advantage of light-weight.
  • a typical material of the latter type is a titanium alloy containing approximately 5% chromium and 3% aluminum as produced by the P. R. Mallory Company; other comparable titanium alloys being produced now by the Remington Company. Currently used high strength ordnance steels may also be used.
  • the muzzle 17 can, if desired, be constructed with a recoil absorbing device, as disclosed in Figure 6.
  • the blast chamber 21 can be formed in several ways, by undercutting from the muzzle end of the barrel or by drilling a hole 22 and inserting a plug 23 therein; the plug 23 having an inside diameter slightly greater than the groove diameter of the bore 11 and being attached by conventional means such as threading 24, and the like.
  • Blast holes 25 are drilled through the barrel 11 to provide gas exit and recoil absorption.
  • Figure 6 shows the plating or hard coating 15 being applied not only to the bore 11 but also to the outside of the barrel.
  • a barrel 26 incorporates a liner 27 constructed of a high strength material.
  • the barrel 26 includes fins 28 about the chamber area for cooling purposes.
  • the liner 27 can be attached to the barrel 26 by conventional means; the attachment shown in Figure 7 including a series of splines 29 to insure proper alignment of the riflings 30 and 31 at the joint 32.
  • the liner 27 is firmly attached to the remaining portion of the barrel by means of threads 33 and coupling 34.
  • the liner 27 can be secured to the barrel proper by direct threading therebetween or by other means.
  • Figure 7 shows, in an exaggerated manner, a plating or hard coating 35 which is comparatively thin, adjacent the chamber of the barrel and which gradually increases in thickness as the 'muzzle is approached.
  • This tapering elfect is advantageous in that the accuracy of the barrel is improved considerably, While permitting the lowering of critical breech pressures.
  • Tapered rifling is also of advantage in that with such a construction a bullet jacket can be fabricated of a harder material, thus allowing greater penetrating power.
  • the taper of the barrel bore is obtained as a result of the hard coating process, as shown by Figure 8.
  • the barrel 26, having a constant bore diameter as a result of machining procedures, is placed within a tank 36 which contains an electrolytic solution 37, as hereinbefore described.
  • the barrel 26 is preferably inserted about a cathode rod 38 which may be negatively charged and which is spaced therefrom by appropriate techniques and means now employed in the plating industry.
  • the barrel 26 may be positively charged to an anode in such a manner that a current flows through the electrolyte 37 to accomplish the formation of the hard coating 35.
  • the barrel can be wholly inserted into the electrolyte and gradually raised or taken out of the bath, by appropriate facilities such as a lifting means 39, thus producing a bore which may be tapered uniformly or non-uniformly in either direction in accordance with the most desired design of barrel.
  • a lifting means 39 thus producing a bore which may be tapered uniformly or non-uniformly in either direction in accordance with the most desired design of barrel.
  • the barrel will be treated uniformly over its whole length.
  • the barrel is preferably transferred to a cold water rinse to remove any residual electrolyte.
  • a firearm barrel of aluminum alloy having an aluminum oxide coating, a metallic coating of copper on said aluminum oxide coating, and a chromium coating on said metallic coating,
  • a firearm barrel of aluminum alloy having an aluminum oxide coating, a metallic coating of nickel on said aluminum oxide coating, and a chromium coating on said metallic coating, where by wear and abrasion are substantially reduced during firing operation.
  • a firearm barrel of aluminum alloy having a metallic coating thereon of copper, and a chromium coating on said metallic coating, said chromium coating being from .001 to .004 inch in thickness, whereby Wear and abrasion are substantially reduced during firing operation.
  • a firearm barrel of aluminum alloy having a metallic coating thereon of nickel, and a chromium coating on said metallic coating, said chromium coating being from .001 to .004 inch in thickness, whereby wear and abrasion are substantially reduced during firing operation.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemically Coating (AREA)

Description

WITH METALLI c ATINGS Feb. 5, 1957 G. c. SULLIVAN GUN BARREL OF ALUMINUM ALLOY Filed Feb. 19, 1952 m&
INVENTOR.
mm mm 2 Sheets-Sheet 2 L mm 3.. mm mm Feb. 5, 1957 G. c. SULLIVAN GUN BARREL OF ALUMINUM ALLOY WITH METALLIC COATINGS Filed Feb. 19, 1952 ternal surface.
United States GUN BARREL F ALUMINUM ALLOY WITH METALLIC COATINGS This invention relates to a firearm or more particularly to a barrel construction wherein the design and materials employed are of such a nature that the resultant product is a minimum in weight. This is accomplished in such a manner that other factors necessary in a practical and successful gun barrel, such as strength and life, are not jeopardized.
The present invention provides a firearm barrel made of a light-weight non-ferrous alloy, preferably aluminum, and including a bore having a plated or hard-coated in: For the purposes of this application, the words coated or coating are to be considered as including the words coated or plated or coating or plating. The present application is a continuation-in-part of my copending application, Serial No. 215,694, filed March 15, 1951, and now abandoned.
The present invention also provides a method of making a firearm barrel, or the like, comprising the steps of machining the barrel from an aluminum alloy blank, drilling a bore axially of the blank, the bore having a diameter slightly in excess of the required finished diameter, and hard-coating the surface of the bore to a dimension that least that required for finished bore diameter. In the case of firearms having low breech pressures, the alloy blank itself may be originally formed in a tubular shape by the use of various well known techniques, thus. integrally containing a bore which can be finished as described hereinafter.
Sportsmen, as well as ordnance manufacturers, have made many attempts to reduce the weight in firearms, for it is recognized that such a light-weight firearm would be advantageous in many respects. Both the sportsman and the soldier will be less fatigued at the end of the day if he has carried less weight. Efforts have been made in the past to decrease action or receiver, stock and sights weight but little, if any, has been attained in reducing barrel weight. This invention discloses a construction and method of manufacture of a gun barrel of reduced weight, yet is of sufficient material cross-section to minimize barrel whip.
As the weight of a firearm is reduced, the recoil normally increases. While it has been found that the increase in recoil is not fatiguing to the average shooter, it may be found desirable to provide a recoil minimizing device. This invention is particularly advantageous in that the decreased weight of the basic material in the barrel will allow a larger barrel cross-section which decreases barrel whip and therefore increases shooting accuracy. This larger barrel cross-section can be carried to the muzzle, thus permitting the use of a muzzle brake or blast device which can be designed into and form a part of the barrel itself. This feature permits a construction that is streamlined, pleasing to the eye in comparison to present devices, economical of manufacture and light in weight. The reduced weight of the basic material used in this invention also allows for a longer barrel which is advantageous in the event of a military weapon and its accompanying bayonet.
mm o
ice
Among the objects achieved in the present invention are the provision of a gun barrel construction in which a non-ferrous alloy is used in conjunction with a hard-plated barrel or bore; a sleeve or liner being incorporated near the chamber of the barrel if desired. The preferred alloy is comprised essentially of aluminum combined with one or more group metals such as zinc, magnesium and copper, For instance, a material discovered to be practical and workable in this application has the following constituents: aluminum 88.5%, magnesium 2.5%, zinc 5.5%, copper 1.5%, chromium 0.30%; the remainder consisting of impurities. Obviously, these metals can be varied within reasonable limits without the resultant material being affected. A preferred material of this type is a wroughtalloy which has received solution heat treatment and elevated temperature aging, and is formed by rolling or preferably by extrusion processes. An alternate aluminum alloy material which may be preferred later is one in which the amount of alloying metals, notably magnesium and zinc, has been increased over that disclosed above. tensile strengths have been increased approximately 8% to date, such material being somewhat experimental in nature atthe present time.
These materials are particularly advantageous in that they are not only light in weight (.10 pound/cubic inch versus .28 pound/cubic inch) when compared to highstrength steels, but have greater thermal conductivity factors (.30 versus .10); the latter fact being of value in the minimization of firing temperatures. This material in combination with cooling fins which may be extruded originally or machined later about the chamber area, Will provide excellent cooling of the barrel.
I have found that a barrel of the above mentioned material will not withstand repeated firing unless a hard-plating is applied to its internal bore. To that end, I propose the use of a chromium or a hard anodic, or the like, plating. For instance, a typical method of chromium plating would be to insert an anode or cathode bar through the bore of the barrel and immerse the combination in an electrolyte for the plating operation; all in accordance with well-known current procedure. The barrel should be anodized first and then ground to remove the oxide below the area to be plated. It may be desirable to give the barrel a flash of copper or nickel to seal the alloy material from water penetration causing corrosion and to prepare a better bonding surface for the chromium plate. The plating is then applied by standard methods. It has been found wise to rotate the barrel during the plating operation to minimize the possibility of uneven plating thickness.
Efiort is made to control the thickness of the plating in order to eliminate subsequent machine operations; however, it is to be understood that the plating can be increased and later reduced to finish dimensions by polishing, grinding, reaming, honing, or the like, machine operations.
Another type of hard-coating has been applied to the bore with great success, such coating being applied by an electrochemical process which creates a non-metallic, hard, heat and corrosion resistant surface which is integral with the base material, not usually requiring the use of a separate plating metal, as described above. One type coating can be created by passing a current through an oxidizing solution, the time of operation and intensity of current determining principally the thickness of the coating obtained, such coating being termed as surface oxidation. A coating recently developed by the Glenn L. Martin Company and described in trade journals, will provide a hard, practical coating for the gun barrel of this invention; such coating having been found to be excellent. Other companies have recently improved their This material is stronger in that the ultimate anodizing treatments to the point that such anodized coating may produce a sufficiently hard, dense and corrosion resistant surface as to be satisfactory. These coatings, usually being composed of amorphous alumina (A1203), offer very gdod resistance to wear and abrasion, and are valuable in that it is highly refractory in nature, offering resistance to high temperatures.
' A coating treatment which has resulted in a fine product consists of an electrolytic bath containing principally sulphuric acid, the temperature of which has been lowered to approximately 30 to 32 F. The use of carbon dioxide as a temperature reducing medium has been found to be excellent in that the carbon dioxide not only performs a refrigerating function but enters into the reaction in such a way thatthe resultant composition of coating has extremely good resistance to wear. Oxalic acid can be added to the bath solution thus permitting higher bath temperatures and resultant lowered costs of operation, but the coating may suffer some in physical characteristics.
'0 The hard coating type of process, distinguishable from the plating process in that the hard coating is formed from the basic material of the barrel itself instead of depositing a plating of another material on the barrel, is advantageous in that there is a surface impregnation which renders a highly efiicient joint action between the hard coating and the basic material of the barrel. In this process a dimensional growth may be associated .with the formation of the hard oxide films, and this feature should be taken into consideration inthe design of the barrel. The oxide surface, although extremely hard, can be finished by honing, lapping, or the like, methods to produce very smooth surfaces.
v A gun barrel when treated according to the process above described has excellent resistance to corrosion and erosion and if designed with taper its performance can be substantially improved.
With the above and other objects in view, those skilled in the art will appreciate the advantages and the invention as disclosed herein, after reviewing the accompanying drawings wherein:
Figure l is a side view of a typical barrel incorporating the present invention, part of Figure 1 being shown in an enlarged and cross-sectioned manner;
Figure 2 is a cross-sectional view of the barrel showing details of the present invention including the provision for a sleeve or liner;
Figure 3 is a sectional view of the barrel showing the plating or coating applied to the bore;
Figure 4 is an elevational cross-sectioned view of the chamber portion of the barrel, showing an alternate liner;
Figure 5 is a sectional view of the barrel showing said alternate liner;
Figure 6 is a sectional view of the muzzle end of the barrel showing an integral recoil minimizing device;
Figure 7 is a sectional view of an alternate design of barrel in which the chamber is incorporated in a liner, cooling fins provided about the chamber area, and the bore being so processed that it is provided with a tapered internal diameter; and
Figure 8 shows a general method of hard plating the barrel and obtaining a tapered bore if desired.
As shown in the drawings, the composite barrel of the present invention includes a barrel body 10 formed of a light-weight material such as aluminum alloy, having the usual bore 11 which may be rifled in the usual manner to provide interior helical-like lands 12. and grooves 13. The barrel It is provided at its rear end with an externally threaded shank 14 or other typical means by which the barrel may be attached to the action or receiver.
The barrel 10, and particularly the bore 11, is coated with a hard coating 15. While it is essential in this invention to coat or plate the bore 11, it is not necessary, however, it may be desirable, to apply a coating to the outside surface of the barrel 10, such coating being accomplished in accordance with procedures outlined herein. The hard coating or plating 15 may be applied to the chamber 16 to assist inpreventing erosion therein, however, I prefer to block off or mask both the chamber 16 and the threads 14 from this operation by using a vinyl tape, or the like, thus preventing interference with prior machining to close tolerances and headspacing of the barrel and action. The barrel can, if desired, be substantially machine finished prior to plating or coating, leaving .001 to .004 inch or less tolerance for the thickness of the coating to be ap' plied.
The rear end of the barrel 10 contains the usual chamber 16, the size and shape of which is determined by the cartridge and caliber used. The explosion pressures are a maximum in the area of the chamber 16 and reduce in the direction of the muzzle 17. While available lightweight metals have been found to have sufiicient strength to withstand with safety the explosion pressures encountered, it may be advisable, if a barrel of exceedingly lowweight is wanted, to incorporate a sleeve 18 around the chamber 16 area where pressures are at a maximum. An alternate sleeve or liner 19 may be incorporated adjacent the chamber 16; this type of strengthening element having the additional advantage of being removable and replaceable in event of excessive erosion due to repeated firing. Both the sleeve 18 and the liner 19 may be installed by sweating the parts together or by furnace brazing, or the like. In the first case, the heat produced as a result of firing tends to increase joint efiiciency action and thus permit each element to absorb its proportion of the stresses produced. The sleeve 18 can drop into detents 20 for security and the liner 19 can be secured by conventional means, such as threading, and the like.
The sleeve 18 or liner 19 is preferably made of a high-strength metal such as stainless steel, which has a tensile strength approaching 125,000 pounds per square inch, or a titanium alloy having a tensile strength in excess of 150,000 pounds per square inch; the latter having the additional advantage of light-weight. A typical material of the latter type is a titanium alloy containing approximately 5% chromium and 3% aluminum as produced by the P. R. Mallory Company; other comparable titanium alloys being produced now by the Remington Company. Currently used high strength ordnance steels may also be used.
The muzzle 17 can, if desired, be constructed with a recoil absorbing device, as disclosed in Figure 6. The blast chamber 21 can be formed in several ways, by undercutting from the muzzle end of the barrel or by drilling a hole 22 and inserting a plug 23 therein; the plug 23 having an inside diameter slightly greater than the groove diameter of the bore 11 and being attached by conventional means such as threading 24, and the like. Blast holes 25 are drilled through the barrel 11 to provide gas exit and recoil absorption. Figure 6 shows the plating or hard coating 15 being applied not only to the bore 11 but also to the outside of the barrel.
The method of manufacture as disclosed by this invention is particularly advantageous in that it lends itself well to the production of a barrel having a tapered bore if so desired, such a tapered bore being obtained in a very economical manner when compared with other fabrication processes. In the alternate design of Figure 7, a barrel 26 incorporates a liner 27 constructed of a high strength material. The barrel 26 includes fins 28 about the chamber area for cooling purposes. The liner 27 can be attached to the barrel 26 by conventional means; the attachment shown in Figure 7 including a series of splines 29 to insure proper alignment of the riflings 30 and 31 at the joint 32. The liner 27 is firmly attached to the remaining portion of the barrel by means of threads 33 and coupling 34. It is to be understood that the liner 27 can be secured to the barrel proper by direct threading therebetween or by other means. Figure 7 shows, in an exaggerated manner, a plating or hard coating 35 which is comparatively thin, adjacent the chamber of the barrel and which gradually increases in thickness as the 'muzzle is approached. This tapering elfect is advantageous in that the accuracy of the barrel is improved considerably, While permitting the lowering of critical breech pressures. Tapered rifling is also of advantage in that with such a construction a bullet jacket can be fabricated of a harder material, thus allowing greater penetrating power.
The taper of the barrel bore is obtained as a result of the hard coating process, as shown by Figure 8. For example, the barrel 26, having a constant bore diameter as a result of machining procedures, is placed Within a tank 36 which contains an electrolytic solution 37, as hereinbefore described. The barrel 26 is preferably inserted about a cathode rod 38 which may be negatively charged and which is spaced therefrom by appropriate techniques and means now employed in the plating industry. The barrel 26 may be positively charged to an anode in such a manner that a current flows through the electrolyte 37 to accomplish the formation of the hard coating 35.
Inasmuch as the formation of the coating is primarily a function of time of immersion, temperature of electrolyte and intensity or density of current applied, it will be seen that by controlling these factors a tapered coating can be easily obtained. For instance the barrel can be wholly inserted into the electrolyte and gradually raised or taken out of the bath, by appropriate facilities such as a lifting means 39, thus producing a bore which may be tapered uniformly or non-uniformly in either direction in accordance with the most desired design of barrel. Of course, if no taper is desired, the barrel will be treated uniformly over its whole length. After treatment the barrel is preferably transferred to a cold water rinse to remove any residual electrolyte.
While a ride barrel has been chosen for illustration and description, it will be understood that the invention is equally applicable to machine guns, shot guns or small arms barrels, such as revolvers or automatics. It may be also applied to other types of firearms or ordnance where reduced Weight is desirable, such as mobile field or tank guns, infantry mortars, recoilless rifles and the like. Smooth bore firearms are well adaptable to this process of manufacture.
It should be apparent that numerous modifications may be made without departing from the spirit of the invention as expressed in the claims.
I claim:
1. A firearm barrel of aluminum alloy, the bore of said barrel having an aluminum oxide coating, a metallic coating of copper on said aluminum oxide coating, and a chromium coating on said metallic coating,
whereby wear and abrasion are substantially reduced during firing operation.
2. A firearm barrel of aluminum alloy, the bore of said barrel having an aluminum oxide coating, a metallic coating of nickel on said aluminum oxide coating, and a chromium coating on said metallic coating, where by wear and abrasion are substantially reduced during firing operation.
3. A firearm barrel of aluminum alloy, the bore of said barrel having a metallic coating thereon of copper, and a chromium coating on said metallic coating, said chromium coating being from .001 to .004 inch in thickness, whereby Wear and abrasion are substantially reduced during firing operation.
4. A firearm barrel of aluminum alloy, the bore of said barrel having a metallic coating thereon of nickel, and a chromium coating on said metallic coating, said chromium coating being from .001 to .004 inch in thickness, whereby wear and abrasion are substantially reduced during firing operation.
References Cited in the file of this patent UNITED STATES PATENTS 660,496 Evans Oct. 23, 1900 785,975 McClean Mar. 28, 1905 817,134 Smith Apr. 3, 1906 1,207,218 Roux 2 Dec. 5, 1918 1,346,190 Fahrenwald July 13, 1920 1,363,058 Schneider Dec. 21, 1920 1,784,325 Witzell Dec. 9, 1930 1,886,218 Olin et a1 Nov. 1, 1932 1,974,429 McCann Sept. 25, 1934 2,104,319 Dicke Jan. 4, 1938 2,112,144 Coupland Mar. 22, 1938 2,129,875 Rost Sept. 13, 1938 2,146,330 Comstock Feb. 7, 1939 2,301,759 Stroup Nov. 10, 1942 2,349,083 Farr May 16, 1944 2,363,563 Vinson Nov. 28, 1944 2,378,959 Vera lune 26, 1945 2,395,044 Gorton Feb. 19, 1946 2,413,022 Wood Dec. 24, 1946 2,423,109 Monnet July 1, 1947 2,440,634 Henney Apr. 27, 1948 2,584,400 Sonnino Feb. 5, 1952 2,687,591 Lamb et al Aug. 31, 1954 2,736,118 Clarkson et a1 Feb. 28, 1956 FOREIGN PATENTS 4,095 Switzerland Sept. 28, 1891 831,030 France .May 30, 1938 233,207
Switzerland Oct. 16, 1944

Claims (1)

1. A FIREARM BARREL OF ALUMINUM ALLOY, THE BORE OF SAID BARREL HAVING AN ALUMINUM OXIDE COATING, A METALLIC COATING OF COPPER ON SAID ALUMINUM OXIDE COATING, AND A CHROMIUM COATING ON SAID METALLIC COATING, WHEREBY WEAR AND ABRASION ARE SUBSTANTIALLY REDUCED DURING FIRING OPERATION.
US272428A 1952-02-19 1952-02-19 Gun barrel of aluminum alloy with metallic coatings Expired - Lifetime US2780019A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US272428A US2780019A (en) 1952-02-19 1952-02-19 Gun barrel of aluminum alloy with metallic coatings
US450442A US2990342A (en) 1952-02-19 1954-08-17 Method of making a gun barrel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US272428A US2780019A (en) 1952-02-19 1952-02-19 Gun barrel of aluminum alloy with metallic coatings

Publications (1)

Publication Number Publication Date
US2780019A true US2780019A (en) 1957-02-05

Family

ID=23039757

Family Applications (1)

Application Number Title Priority Date Filing Date
US272428A Expired - Lifetime US2780019A (en) 1952-02-19 1952-02-19 Gun barrel of aluminum alloy with metallic coatings

Country Status (1)

Country Link
US (1) US2780019A (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930252A (en) * 1959-03-23 1960-03-29 Beaver Prec Products Inc Valve operator
US2935913A (en) * 1956-04-24 1960-05-10 Olin Mathieson Gun barrel
US3051632A (en) * 1959-07-27 1962-08-28 William D Kraemer Method of electroplating copper elbows
US3261121A (en) * 1961-10-13 1966-07-19 Joseph R Eves Gun barrel with explosively welded liner
US3398476A (en) * 1966-10-20 1968-08-27 Hoving Tore Erik Firearm with a breech bolt having a swingable action end with an extractor attached thereto
US4474651A (en) * 1981-08-20 1984-10-02 Sumitomo Metal Industries, Ltd. Oil well casing and tubing joint and production of same
WO1986002719A1 (en) * 1984-10-29 1986-05-09 General Electric Company Gun barrel for use at high temperature
US4649797A (en) * 1981-06-04 1987-03-17 Rheinmetall Gmbh Gun barrel with reduced, repeative jump angle
US5341719A (en) * 1992-12-14 1994-08-30 General Electric Company Multi-layer composite gun barrel
US20070193102A1 (en) * 2006-02-23 2007-08-23 Briggs Vernon R Composite firearm barrel
US20070261286A1 (en) * 2006-02-23 2007-11-15 Sturm, Ruger & Company, Inc. Composite firearm barrel reinforcement
US8834699B1 (en) * 2006-04-27 2014-09-16 Tantalum Pellet Co. Method of anodizing
US20150082679A1 (en) * 2013-09-23 2015-03-26 Frank MICHAL Firearm barrel sleeves and barrel grips
US20220042758A1 (en) * 2017-06-01 2022-02-10 Willow Associates, LLC Machine Gun Infantry "KT-7.62"
US20230074469A1 (en) * 2021-09-08 2023-03-09 Brown Dog Intellectual Properties Extended life composite matrix-wrapped lightweight firearm barrel

Citations (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH4095A (en) * 1891-09-28 1892-02-15 Rudolf Elmer Gun barrel with feed barrel
US660496A (en) * 1899-07-15 1900-10-23 William S Evans Gun-barrel.
US785975A (en) * 1904-07-01 1905-03-28 Samuel N Mcclean Means for controlling the recoil and muzzle-blast of guns.
US817134A (en) * 1903-02-21 1906-04-03 William Davidson Condit Gun.
US1207218A (en) * 1914-01-19 1916-12-05 L Aluminium Francais Soc Process of producing metallic deposits.
US1346190A (en) * 1919-12-15 1920-07-13 Frank A Fahrenwald Firearm and alloy for making same
US1363058A (en) * 1921-02-10 1920-12-21 T F Shanahn Car construction
US1784325A (en) * 1928-06-01 1930-12-09 Rheinische Metallw & Maschf Barrel of firearms
US1886218A (en) * 1927-06-29 1932-11-01 Western Cartridge Co Gun barrel and process of finishing the same
US1974429A (en) * 1932-04-21 1934-09-25 George M Mccann Gun
US2104319A (en) * 1934-02-10 1938-01-04 Remington Arms Co Inc Manufacture of rifled tubes
US2112144A (en) * 1932-07-28 1938-03-22 Secretary Of War Of The United Means for cooling gun barrels
FR831030A (en) * 1937-04-01 1938-08-18 Barrel for rifles or other weapons
US2129875A (en) * 1935-05-25 1938-09-13 Rost Helge Ammunition and firearm
US2146330A (en) * 1937-02-18 1939-02-07 Titanium Alloy Mfg Co Aluminum-zinc alloys
US2301759A (en) * 1940-09-05 1942-11-10 Aluminum Co Of America Aluminum alloy rivet
US2349083A (en) * 1940-05-13 1944-05-16 B & T Floor Company Electrolytic process for coating aluminum and aluminum alloys
CH233207A (en) * 1942-02-08 1944-07-15 Rheinmetall Borsig Ag Gun barrel.
US2363563A (en) * 1942-11-18 1944-11-28 Neal L Vinson Air-cooled gun barrel
US2378959A (en) * 1942-12-18 1945-06-26 Francis L Vera Gun barrel
US2395044A (en) * 1942-04-02 1946-02-19 Walter T Gorton Gun
US2413022A (en) * 1943-09-22 1946-12-24 George A Woody Method of forming firearm barrels
US2423109A (en) * 1944-07-01 1947-07-01 Monnet Georges Means for improving the ejection of masses
US2440634A (en) * 1943-10-14 1948-04-27 Gen Motors Corp Shell feeding mechanism for rocket guns
US2584400A (en) * 1944-10-20 1952-02-05 Sonnino Carlo Process for anodic oxidation of aluminum and its alloys
US2687591A (en) * 1949-10-31 1954-08-31 Us Army Rifled gun barrel with tapered chromium bore wall
US2736118A (en) * 1951-12-18 1956-02-28 Firearm with chamber member remov-

Patent Citations (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH4095A (en) * 1891-09-28 1892-02-15 Rudolf Elmer Gun barrel with feed barrel
US660496A (en) * 1899-07-15 1900-10-23 William S Evans Gun-barrel.
US817134A (en) * 1903-02-21 1906-04-03 William Davidson Condit Gun.
US785975A (en) * 1904-07-01 1905-03-28 Samuel N Mcclean Means for controlling the recoil and muzzle-blast of guns.
US1207218A (en) * 1914-01-19 1916-12-05 L Aluminium Francais Soc Process of producing metallic deposits.
US1346190A (en) * 1919-12-15 1920-07-13 Frank A Fahrenwald Firearm and alloy for making same
US1363058A (en) * 1921-02-10 1920-12-21 T F Shanahn Car construction
US1886218A (en) * 1927-06-29 1932-11-01 Western Cartridge Co Gun barrel and process of finishing the same
US1784325A (en) * 1928-06-01 1930-12-09 Rheinische Metallw & Maschf Barrel of firearms
US1974429A (en) * 1932-04-21 1934-09-25 George M Mccann Gun
US2112144A (en) * 1932-07-28 1938-03-22 Secretary Of War Of The United Means for cooling gun barrels
US2104319A (en) * 1934-02-10 1938-01-04 Remington Arms Co Inc Manufacture of rifled tubes
US2129875A (en) * 1935-05-25 1938-09-13 Rost Helge Ammunition and firearm
US2146330A (en) * 1937-02-18 1939-02-07 Titanium Alloy Mfg Co Aluminum-zinc alloys
FR831030A (en) * 1937-04-01 1938-08-18 Barrel for rifles or other weapons
US2349083A (en) * 1940-05-13 1944-05-16 B & T Floor Company Electrolytic process for coating aluminum and aluminum alloys
US2301759A (en) * 1940-09-05 1942-11-10 Aluminum Co Of America Aluminum alloy rivet
CH233207A (en) * 1942-02-08 1944-07-15 Rheinmetall Borsig Ag Gun barrel.
US2395044A (en) * 1942-04-02 1946-02-19 Walter T Gorton Gun
US2363563A (en) * 1942-11-18 1944-11-28 Neal L Vinson Air-cooled gun barrel
US2378959A (en) * 1942-12-18 1945-06-26 Francis L Vera Gun barrel
US2413022A (en) * 1943-09-22 1946-12-24 George A Woody Method of forming firearm barrels
US2440634A (en) * 1943-10-14 1948-04-27 Gen Motors Corp Shell feeding mechanism for rocket guns
US2423109A (en) * 1944-07-01 1947-07-01 Monnet Georges Means for improving the ejection of masses
US2584400A (en) * 1944-10-20 1952-02-05 Sonnino Carlo Process for anodic oxidation of aluminum and its alloys
US2687591A (en) * 1949-10-31 1954-08-31 Us Army Rifled gun barrel with tapered chromium bore wall
US2736118A (en) * 1951-12-18 1956-02-28 Firearm with chamber member remov-

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2935913A (en) * 1956-04-24 1960-05-10 Olin Mathieson Gun barrel
US2930252A (en) * 1959-03-23 1960-03-29 Beaver Prec Products Inc Valve operator
US3051632A (en) * 1959-07-27 1962-08-28 William D Kraemer Method of electroplating copper elbows
US3261121A (en) * 1961-10-13 1966-07-19 Joseph R Eves Gun barrel with explosively welded liner
US3398476A (en) * 1966-10-20 1968-08-27 Hoving Tore Erik Firearm with a breech bolt having a swingable action end with an extractor attached thereto
US4649797A (en) * 1981-06-04 1987-03-17 Rheinmetall Gmbh Gun barrel with reduced, repeative jump angle
US4474651A (en) * 1981-08-20 1984-10-02 Sumitomo Metal Industries, Ltd. Oil well casing and tubing joint and production of same
WO1986002719A1 (en) * 1984-10-29 1986-05-09 General Electric Company Gun barrel for use at high temperature
US4669212A (en) * 1984-10-29 1987-06-02 General Electric Company Gun barrel for use at high temperature
JPH068720B2 (en) * 1984-10-29 1994-02-02 ゼネラル・エレクトリック・カンパニイ Barrel for use under high temperature and manufacturing method thereof
US5341719A (en) * 1992-12-14 1994-08-30 General Electric Company Multi-layer composite gun barrel
US20070261286A1 (en) * 2006-02-23 2007-11-15 Sturm, Ruger & Company, Inc. Composite firearm barrel reinforcement
US20070193102A1 (en) * 2006-02-23 2007-08-23 Briggs Vernon R Composite firearm barrel
US7921590B2 (en) 2006-02-23 2011-04-12 Strum, Ruger & Company, Inc. Composite firearm barrel reinforcement
US7934332B2 (en) 2006-02-23 2011-05-03 Sturm, Ruger & Company, Inc. Composite firearm barrel
US8316568B2 (en) 2006-02-23 2012-11-27 Sturm, Ruger & Company, Inc. Composite firearm barrel reinforcement
US8834699B1 (en) * 2006-04-27 2014-09-16 Tantalum Pellet Co. Method of anodizing
EP2167900A2 (en) * 2007-07-18 2010-03-31 Sturm, Ruger & Company, Inc. Composite firearm barrel reinforcement
EP2167900A4 (en) * 2007-07-18 2011-09-14 Sturm Ruger & Co Composite firearm barrel reinforcement
US20150082679A1 (en) * 2013-09-23 2015-03-26 Frank MICHAL Firearm barrel sleeves and barrel grips
US9239202B2 (en) * 2013-09-23 2016-01-19 Frank MICHAL Firearm barrel sleeves and barrel grips
US20220042758A1 (en) * 2017-06-01 2022-02-10 Willow Associates, LLC Machine Gun Infantry "KT-7.62"
US11774204B2 (en) * 2017-06-01 2023-10-03 Willow Associates, LLC Machine gun infantry “KT-7.62”
US20230074469A1 (en) * 2021-09-08 2023-03-09 Brown Dog Intellectual Properties Extended life composite matrix-wrapped lightweight firearm barrel

Similar Documents

Publication Publication Date Title
US2850828A (en) Aluminum alloy gun barrel with a lubricating film
US2780019A (en) Gun barrel of aluminum alloy with metallic coatings
US2990342A (en) Method of making a gun barrel
US4577431A (en) Wear resistant gun barrel and method of forming
US4669212A (en) Gun barrel for use at high temperature
US3027672A (en) Firearm with aluminum alloy receiver
US1886218A (en) Gun barrel and process of finishing the same
US3498221A (en) Aluminum cartridge case
US20100236122A1 (en) Flowforming Gun Barrels and Similar Tubular Devices
US20140305019A1 (en) Magnesium firearm forearm and method of manufacture
US4622080A (en) Gun barrel, mandrel and related processes
US2926612A (en) Projectile
EP1183121B1 (en) Blank for gunbarrel, method for producing said gunbarrel and gunbarrel
US2196018A (en) Cartridge case provided with a nonmetallic surface
RU2557892C2 (en) Method of production of gun barrel
US10633719B1 (en) Gun barrel manufacturing methods
US3442172A (en) Gun barrel liner
US2687591A (en) Rifled gun barrel with tapered chromium bore wall
US2395044A (en) Gun
US2799959A (en) Nitrided gun barrel with chromium deposit
CN103615929A (en) Composite gun barrel material for small-caliber antiaircraft gun or close-in gun and manufacturing method thereof
US8333029B1 (en) Extreme duty machine gun barrel
US2636849A (en) Method of electroforming gun barrels and liners
US20100282369A1 (en) Noveske rifleworks extreme duty machine gun barrel
US3112553A (en) Electroforming of gun liners