US2499944A - Gun tube liner material - Google Patents
Gun tube liner material Download PDFInfo
- Publication number
- US2499944A US2499944A US701298A US70129846A US2499944A US 2499944 A US2499944 A US 2499944A US 701298 A US701298 A US 701298A US 70129846 A US70129846 A US 70129846A US 2499944 A US2499944 A US 2499944A
- Authority
- US
- United States
- Prior art keywords
- liner
- tube
- mandrel
- split
- gun tube
- 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
Links
- 239000000463 material Substances 0.000 title description 11
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 238000004049 embossing Methods 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 2
- AFTDTIZUABOECB-UHFFFAOYSA-N [Co].[Mo] Chemical compound [Co].[Mo] AFTDTIZUABOECB-UHFFFAOYSA-N 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 239000011733 molybdenum Substances 0.000 description 2
- DDTIGTPWGISMKL-UHFFFAOYSA-N molybdenum nickel Chemical compound [Ni].[Mo] DDTIGTPWGISMKL-UHFFFAOYSA-N 0.000 description 2
- MGRWKWACZDFZJT-UHFFFAOYSA-N molybdenum tungsten Chemical compound [Mo].[W] MGRWKWACZDFZJT-UHFFFAOYSA-N 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 238000004873 anchoring Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/16—Barrels or gun tubes characterised by the shape of the bore
- F41A21/18—Grooves-Rifling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/02—Composite barrels, i.e. barrels having multiple layers, e.g. of different materials
- F41A21/04—Barrel liners
Definitions
- This invention relates to a liner for gun tubes, and particularly to a thin liner of resistant metal such as molybdenum, molybdenum-tungsten, molybdenum-cobalt and molybdenum-nickel alloys, tungsten and the like, as well as means for anchoring the resistant metal in the gun tube, and means for rifling the liner tube.
- resistant metal such as molybdenum, molybdenum-tungsten, molybdenum-cobalt and molybdenum-nickel alloys, tungsten and the like
- An object of our invention is to provide a gun tube lined with a sheet of metal resistant to high temperteures, wear and chemical erosion, with means for securely retaining said liner. Another object is to provide means for riiling a lined gun tube by embossing.
- Figure 2 is a perspective cross section view of the liner assembled with a split liner retaining tube
- Figure 3 is a perspective cross section view of the completely assembled gun tube
- Figure 4 is a perspective cross section view of a mandrel for embossing the rifling on the liner in the gun tube,
- Figure 5 is a perspective cross section View showing the mandrel in the gun tube
- Figure 6 is a longitudinal cross section view showing the mandrel in the gun tube
- Figure 7 is a perspective view of a modification showing helical liner sections.
- Two sheets or strips of resistant metal such as molybdenum, molybdenum-tungsten, molybdenum-cobalt and molybdenum-nickel alloys and tungsten or the like are formed into liners of ilanged semi-cylindrical shape as shown in I.-I in Figure 1 and are then assembled with semi-cylinders 3'3 whose radial thickness corresponds to the width of anges 2 of the liner l-i.
- a tube (not shown) of extensible or plastic material suchas copper or the like may be positioned within the split mandrel 5 and hydraulic pressure is thereafter applied internally of the tube in any suitable manner to eflectvan expansion of the copper tube and force the split mandrel 5 into embossing engagement with the liner of resistant metal forming the bore.
- the gun tube having the liner therein may be swaged directly onto the split mandrel 5 and the swaging operation may be performedeither hot or cold to emboss the riing grooves onto the bore of the gun tube.
- the mandrell may be made of a low expansivity material, so
- Reinforced metal tubing comprising an 1 outer tube, a split inner tube of substantial radial thickness firmly held within said outer tube, and a split liner of thin resistant material, each section of which has radially upturned flanges held between adjacent sections of said -split inner engagement therewith, a split liner of sheet material, each section of which has flanges extending radially toward the outer tube for a distance corresponding to the thickness of said split inner tube and between adjacent sections of said liner tube, whereby the adjacent anges of each two adjacent section of said split liner are held between two adjacent sections of said split inner tube.
- the method of forming a gun tube having a thin liner of resistant material which comprises; forming strips of said resistant material into liner sections having radial anges extending outwardly from the inner tube surface, assembling said liner section with adjacent flanges in side by side abutting relationship, forming a spilt mbe of manantial mami tmcness with sea tions corresponding to the. ⁇ said liner section, assembling said split tube about said liner section so that the adjacent radial edges of said split tube serve to clamp abutting flanges of said liner sections, and forcing said assembly into frictional engagement with an outer tube to hold said assemblytogether.
- the method offorming a riiied gun tube having a thin liner of resistant material which comprises; forming strips of resistant material into linerv sections having radially upturned edges, clamping/the radially upturned edges on each said strip between-adjacent sectionsl of a split rigid inner liner, forcing said assembly into frictional engagement with an outer ⁇ tube to hold said assembly together, inserting intothe barrel a split mandrel consisting of sections correspondi'ng to the liner sections, each mandrel section being providewith projecting means to produce one or. more rifling grooves, and forcing said mandrel sections against thel inner surface of said gun barrel to produce rifling corresponding in longitudinal direction to the longitudinal direction of the said liner sections.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Forging (AREA)
Description
I Patented Mar. 7, 1950 FICE GUN TUBE LINER MATERIAL Porter H. Brace, Forest Hills. Pa., John Frank Schalrer, Chevy Chase, Md., and John W.
Marden,
ast Orange, N. J., assgnors to the United States of America asv represented by the Secretary of War Application October 4, 1946,`Serial No. 701,298
6 Claims. (Cl. Sii-16) This invention relates to a liner for gun tubes, and particularly to a thin liner of resistant metal such as molybdenum, molybdenum-tungsten, molybdenum-cobalt and molybdenum-nickel alloys, tungsten and the like, as well as means for anchoring the resistant metal in the gun tube, and means for rifling the liner tube.
An object of our invention is to provide a gun tube lined with a sheet of metal resistant to high temperteures, wear and chemical erosion, with means for securely retaining said liner. Another object is to provide means for riiling a lined gun tube by embossing.
The'manner in which the above and other objects are attained is disclosed in the specilication and the appended drawings in which,A Y Figure 1 is a .perspective cross section view of the liner` of the resistant metal,
Figure 2 is a perspective cross section view of the liner assembled with a split liner retaining tube,
Figure 3 is a perspective cross section view of the completely assembled gun tube,
Figure 4 is a perspective cross section view of a mandrel for embossing the rifling on the liner in the gun tube,
Figure 5 is a perspective cross section View showing the mandrel in the gun tube,
Figure 6 is a longitudinal cross section view showing the mandrel in the gun tube,
Figure 7 is a perspective view of a modification showing helical liner sections.
Two sheets or strips of resistant metal such as molybdenum, molybdenum-tungsten, molybdenum-cobalt and molybdenum-nickel alloys and tungsten or the like are formed into liners of ilanged semi-cylindrical shape as shown in I.-I in Figure 1 and are then assembled with semi-cylinders 3'3 whose radial thickness corresponds to the width of anges 2 of the liner l-i.
The assembly shown in Figure 2 is then intrically disposed tube elements are old'in the art and we do not broadly make any claim to this feature. l
In order to provide rifling in the gun tube bore as described above, without removing any material from the thin liner and thus weakening same, we prefer to emboss or impress the riing upon the inside surface of the assembled tube. For this purpose we make use of a suitably hardened mandrel 5, split into several elements G, as shown in Figure 4. A tapered mandrel spacer 1 is-provided to force the split elements 6, into embossing or swaging engagement with the liner. The inner surfaces of the mandrel element are shaped to conform to the taper of the mandrel spacer. The longitudinally split mandrel construction also facilitates the removal of the mandrel after the swaging operation is completed.
As an alternative for the taperedv mandrel a tube (not shown) of extensible or plastic material suchas copper or the like may be positioned within the split mandrel 5 and hydraulic pressure is thereafter applied internally of the tube in any suitable manner to eflectvan expansion of the copper tube and force the split mandrel 5 into embossing engagement with the liner of resistant metal forming the bore. As a further alternative, the gun tube having the liner therein may be swaged directly onto the split mandrel 5 and the swaging operation may be performedeither hot or cold to emboss the riing grooves onto the bore of the gun tube.
closed in a tube I as shown in Figure 3, by shrink f It is desirable that the joints between the sections of the assembled gun tube conform in direction to the direction of the riiiing. This may be effected by preforming the sections to a helical shape as shown in Figure 7, wherein the same reference numeral with the subscript a added low the same corresponding parts as in the Figure 2. While we have shown a two section inner assembly it is to be understood that our invention also comprehends the use of several helical sections, each part bearing one land of the riling. The inner assembly may thus be built up of identical components.
With this helical construction, the further advantage is obtained that rotation of the bullet due to the rifling does not cause the bullet survface to rub circumferentially against the :lunction of adjacent sections of the liner I, with consequent tearing tendency, but only adds to the riiling eilect. It is contemplated, however, that the closeness of it, together with the swaging operation will be effective to reduce the crevices at the junction of adjacent liner sections to aminimum, so that a substantially continuous inner surface will be formed by the lin tions. To facilitate removal of the mandrel after the embossing operation is completed, the mandrell may be made of a low expansivity material, so
' that heating of the gun tube will tend to free it from the mandrel.
We claim:
1. Reinforced metal tubing comprising an 1 outer tube, a split inner tube of substantial radial thickness firmly held within said outer tube, and a split liner of thin resistant material, each section of which has radially upturned flanges held between adjacent sections of said -split inner engagement therewith, a split liner of sheet material, each section of which has flanges extending radially toward the outer tube for a distance corresponding to the thickness of said split inner tube and between adjacent sections of said liner tube, whereby the adjacent anges of each two adjacent section of said split liner are held between two adjacent sections of said split inner tube.
5. The method of forming a gun tube having a thin liner of resistant material which comprises; forming strips of said resistant material into liner sections having radial anges extending outwardly from the inner tube surface, assembling said liner section with adjacent flanges in side by side abutting relationship, forming a spilt mbe of manantial mami tmcness with sea tions corresponding to the.` said liner section, assembling said split tube about said liner section so that the adjacent radial edges of said split tube serve to clamp abutting flanges of said liner sections, and forcing said assembly into frictional engagement with an outer tube to hold said assemblytogether. f
6. The method offorming a riiied gun tube having a thin liner of resistant material which comprises; forming strips of resistant material into linerv sections having radially upturned edges, clamping/the radially upturned edges on each said strip between-adjacent sectionsl of a split rigid inner liner, forcing said assembly into frictional engagement with an outer` tube to hold said assembly together, inserting intothe barrel a split mandrel consisting of sections correspondi'ng to the liner sections, each mandrel section being providewith projecting means to produce one or. more rifling grooves, and forcing said mandrel sections against thel inner surface of said gun barrel to produce rifling corresponding in longitudinal direction to the longitudinal direction of the said liner sections.
PORTER H. BRACE.
JOHN-FRANK SCHAIRER. JOHN W. MARDEN.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Great Britain Apr. 28, 1883
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US701298A US2499944A (en) | 1946-10-04 | 1946-10-04 | Gun tube liner material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US701298A US2499944A (en) | 1946-10-04 | 1946-10-04 | Gun tube liner material |
Publications (1)
Publication Number | Publication Date |
---|---|
US2499944A true US2499944A (en) | 1950-03-07 |
Family
ID=24816802
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US701298A Expired - Lifetime US2499944A (en) | 1946-10-04 | 1946-10-04 | Gun tube liner material |
Country Status (1)
Country | Link |
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US (1) | US2499944A (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2609631A (en) * | 1948-05-24 | 1952-09-09 | John C Garand | Means for securing liners to firearm barrels |
US2789428A (en) * | 1952-07-24 | 1957-04-23 | Mackas George | Gun tube temperature simulator |
US2820399A (en) * | 1952-11-05 | 1958-01-21 | Comenetz George | Offset half ring molybdenum gun liners |
US2849923A (en) * | 1954-09-30 | 1958-09-02 | Crane Co | Gun barrel liner |
US2901814A (en) * | 1956-04-02 | 1959-09-01 | George C Sullivan | Method of manufacturing gun barrels |
US2915946A (en) * | 1951-10-30 | 1959-12-08 | Westinghouse Electric Corp | Segmented molybdenum gun liner |
US2972179A (en) * | 1952-07-29 | 1961-02-21 | Stuart V Cuthbert | Method for producing molybdenum or molybdenum alloy gun liner |
US2977666A (en) * | 1954-12-29 | 1961-04-04 | Porter H Brace | Method of making gun liner elements |
US2985946A (en) * | 1955-05-10 | 1961-05-30 | Philips Corp | Indirectly heated cathode |
US3010398A (en) * | 1957-10-15 | 1961-11-28 | Parlanti Conrad Anthony | Composite nose cone structure |
US3025765A (en) * | 1952-01-30 | 1962-03-20 | Westinghouse Electric Corp | Segmented ring-type refractory metal liners for guns |
US3136084A (en) * | 1962-03-09 | 1964-06-09 | Smith And Wesson Inc | Gas cutting prevention in revolver firearms |
US3523035A (en) * | 1966-12-21 | 1970-08-04 | Texas Instruments Inc | Internally coated gun barrels |
US5212328A (en) * | 1991-10-11 | 1993-05-18 | Petrovich Paul A | Nonmetallic gun barrel |
US20170205172A1 (en) * | 2016-01-14 | 2017-07-20 | Proof Research, Inc. | Composite multi-lobe projectile barrel |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1748272A (en) * | 1926-03-26 | 1930-02-25 | Gladeon M Barnes | Ordnance |
US1789308A (en) * | 1927-07-25 | 1931-01-20 | James L Hatcher | Apparatus for rifling gun barrels |
US2383356A (en) * | 1944-04-05 | 1945-08-21 | Remington Arms Co Inc | Firearm |
-
1946
- 1946-10-04 US US701298A patent/US2499944A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1748272A (en) * | 1926-03-26 | 1930-02-25 | Gladeon M Barnes | Ordnance |
US1789308A (en) * | 1927-07-25 | 1931-01-20 | James L Hatcher | Apparatus for rifling gun barrels |
US2383356A (en) * | 1944-04-05 | 1945-08-21 | Remington Arms Co Inc | Firearm |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2609631A (en) * | 1948-05-24 | 1952-09-09 | John C Garand | Means for securing liners to firearm barrels |
US2915946A (en) * | 1951-10-30 | 1959-12-08 | Westinghouse Electric Corp | Segmented molybdenum gun liner |
US3025765A (en) * | 1952-01-30 | 1962-03-20 | Westinghouse Electric Corp | Segmented ring-type refractory metal liners for guns |
US2789428A (en) * | 1952-07-24 | 1957-04-23 | Mackas George | Gun tube temperature simulator |
US2972179A (en) * | 1952-07-29 | 1961-02-21 | Stuart V Cuthbert | Method for producing molybdenum or molybdenum alloy gun liner |
US2820399A (en) * | 1952-11-05 | 1958-01-21 | Comenetz George | Offset half ring molybdenum gun liners |
US2849923A (en) * | 1954-09-30 | 1958-09-02 | Crane Co | Gun barrel liner |
US2977666A (en) * | 1954-12-29 | 1961-04-04 | Porter H Brace | Method of making gun liner elements |
US2985946A (en) * | 1955-05-10 | 1961-05-30 | Philips Corp | Indirectly heated cathode |
US2901814A (en) * | 1956-04-02 | 1959-09-01 | George C Sullivan | Method of manufacturing gun barrels |
US3010398A (en) * | 1957-10-15 | 1961-11-28 | Parlanti Conrad Anthony | Composite nose cone structure |
US3136084A (en) * | 1962-03-09 | 1964-06-09 | Smith And Wesson Inc | Gas cutting prevention in revolver firearms |
US3523035A (en) * | 1966-12-21 | 1970-08-04 | Texas Instruments Inc | Internally coated gun barrels |
US5212328A (en) * | 1991-10-11 | 1993-05-18 | Petrovich Paul A | Nonmetallic gun barrel |
US20170205172A1 (en) * | 2016-01-14 | 2017-07-20 | Proof Research, Inc. | Composite multi-lobe projectile barrel |
US10001337B2 (en) * | 2016-01-14 | 2018-06-19 | Proof Research, Inc. | Composite multi-lobe projectile barrel |
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