EP0114593A1 - Verfahren zur Herstellung eines Maschinenhohlzylinders für Kunststoffverarbeitungsmaschinen - Google Patents
Verfahren zur Herstellung eines Maschinenhohlzylinders für Kunststoffverarbeitungsmaschinen Download PDFInfo
- Publication number
- EP0114593A1 EP0114593A1 EP83890234A EP83890234A EP0114593A1 EP 0114593 A1 EP0114593 A1 EP 0114593A1 EP 83890234 A EP83890234 A EP 83890234A EP 83890234 A EP83890234 A EP 83890234A EP 0114593 A1 EP0114593 A1 EP 0114593A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- tube
- jacket tube
- resistant
- hollow cylinder
- alloy
- 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.)
- Withdrawn
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 6
- 238000000034 method Methods 0.000 title claims description 12
- 239000000463 material Substances 0.000 claims abstract description 23
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 13
- 239000000956 alloy Substances 0.000 claims abstract description 13
- 238000005242 forging Methods 0.000 claims abstract description 8
- 238000010438 heat treatment Methods 0.000 claims abstract description 6
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 4
- 238000002844 melting Methods 0.000 claims abstract description 4
- 230000008018 melting Effects 0.000 claims abstract description 4
- 239000010959 steel Substances 0.000 claims abstract description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract 4
- 229910052759 nickel Inorganic materials 0.000 claims abstract 2
- 238000012856 packing Methods 0.000 claims abstract 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 14
- 239000002775 capsule Substances 0.000 claims description 9
- 239000002131 composite material Substances 0.000 claims description 7
- 229910052742 iron Inorganic materials 0.000 claims description 7
- 239000004033 plastic Substances 0.000 claims description 6
- 229920003023 plastic Polymers 0.000 claims description 6
- 229910000531 Co alloy Inorganic materials 0.000 claims description 3
- 229910000915 Free machining steel Inorganic materials 0.000 claims description 3
- 239000002318 adhesion promoter Substances 0.000 claims description 3
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 239000000945 filler Substances 0.000 claims description 3
- 239000007769 metal material Substances 0.000 claims description 3
- 229910000669 Chrome steel Inorganic materials 0.000 claims description 2
- 239000012298 atmosphere Substances 0.000 claims description 2
- 238000005253 cladding Methods 0.000 claims description 2
- 238000005260 corrosion Methods 0.000 claims description 2
- 230000007797 corrosion Effects 0.000 claims description 2
- 238000003754 machining Methods 0.000 claims description 2
- 230000001681 protective effect Effects 0.000 claims description 2
- 229910017052 cobalt Inorganic materials 0.000 abstract description 3
- 239000010941 cobalt Substances 0.000 abstract description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 abstract description 3
- 150000001875 compounds Chemical class 0.000 abstract 2
- 239000000843 powder Substances 0.000 description 9
- 239000000203 mixture Substances 0.000 description 6
- 239000011651 chromium Substances 0.000 description 5
- 229910000746 Structural steel Inorganic materials 0.000 description 3
- 238000001513 hot isostatic pressing Methods 0.000 description 3
- 229910001220 stainless steel Inorganic materials 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 239000012300 argon atmosphere Substances 0.000 description 2
- 238000007872 degassing Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000005272 metallurgy Methods 0.000 description 2
- 238000004873 anchoring Methods 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/12—Both compacting and sintering
- B22F3/1208—Containers or coating used therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/08—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
- Y10T428/12063—Nonparticulate metal component
- Y10T428/12097—Nonparticulate component encloses particles
Definitions
- a composite material has proven itself, which is formed as a hollow cylinder from a forged or hot-rolled blank from a highly wear-resistant, hardenable and corrosion-resistant steel core and a shell made of structural steel.
- the object of the present invention is now to provide a method which allows a machine hollow cylinder for plastic processing machines to be produced in a particularly simple manner, with a high possibility of combination for the different materials, depending on the application, being given.
- the inventive method for producing a Ma . schin hollow cylinder for plastics processing machines with an outer tube and an inner tube of a different material essentially consists in that in a H lenrohr ül- which is optionally disposed in a capsule tube, of a tenacious alloy such as steel, a filling of a bulk density of at least 60 % of the density of the compact, powdery, highly wear-resistant, in particular highly heat-wear-resistant and / or corrosion-resistant material, optionally in the pre-pressed and / or pre-sintered state and preferably with the exception of one, in particular central, hollow area of the jacket tube, is introduced, optionally compressed, and on the jacket tube ends respectively.
- the central hollow area is filled with a filler, preferably made of an easily machinable material, e.g. Free cutting steel, so on the one hand elaborate powder is saved, and at the same time a particularly simple manufacture of an inner hollow can be carried out.
- a filler preferably made of an easily machinable material, e.g. Free cutting steel
- a tube can also be used as a filler body, where it is then forged using a mandrel, for example, and additional labor savings can occur.
- the composite body is subjected to a hot deformation, in particular forging, with a deformation of at least 1.3, in particular 2 times, before it is mechanically processed into a hollow machine cylinder, in addition to the particularly high metallurgical bond between the powder-metallurgically solidified material and the melt-metallurgically obtained tube, there is an additional increase the mechanical properties of the powder metallurgical material is achieved, so that there is another field of application.
- a difficult-to-deform iron-based alloy in particular a ledeburitic chromium steel, can be used as the material for filling the casing tube, in which case the advantages of the method according to the invention become particularly clear.
- a cobalt-based alloy is also particularly suitable as a highly wear-resistant alloy.
- the cladding tube can have an inner coating made of an adhesion promoter in order to achieve better anchoring of the powder metallurgical material in the tube obtained by melting metallurgy.
- a sleeve tube made of an alloy of the following composition in wt .-% C 0.26, Si 0.30, Mn 0.70, Cr 1.1, Mo 0.25 and remainder iron with an outer diameter of 210 mm and an inner diameter of 85 mm and a length of 900 mm.
- a powder of a ledeburitic chromium steel alloy with the following composition in% by weight of C 2.3, Si 0.28, Mn 0.37, Cr 12.6, Mo 0.98, V 4.1 and the rest iron was filled into this tube , wherein a density of 5.2 g / cm 3 was achieved by shaking.
- Degassing was carried out at 360 ° C., whereupon an upper cover with a suction opening was welded onto the capsule tube. Then it was evacuated and the suction opening was closed.
- the encapsulated body was hot-isostatically pressed for 3 hours in an argon atmosphere at 1050 ° C. and at a pressure of 1000 bar.
- This composite body was then forged on a long forging machine to an outside diameter of approx. 85 mm, which corresponds to an approx. 6, lfold deformation. After forging was annealed, followed by an extruder cylinder was manufactured by mechanical processing, cutting to length, turning and heat treatment.
- a machine hollow cylinder for plastic processing machines was produced in such a way that a cylindrical sleeve tube made of 16MnCr5 with an outer diameter of 85 mm, an inner diameter of 45 mm and a length of 650 mm with a spherical powder formed from the melt and having a bulk density of about 66% from a ledeburitic chromium steel alloy of the composition in% by weight C 2.2, Si 0.28, Mn 0.37, Cr 12.6, Mo 0.98, V 4.1, the rest essentially filled with iron Evacuation was compressed and sealed gas-tight at the pipe ends by means of welded-on round cover plates.
- the blank was then placed in a hot isostatic pressing device and subjected to a temperature of 1060 ° C and an argon gas pressure of 1000 bar for three hours, and then cooled to room temperature in still air. After the plates had been cut off by sawing off the two outermost pipe ends, the hollow of 24 mm in diameter was formed using a hole boring machine and heat-treated.
- a cylinder for plastic processing machines was produced analogously to Example 1, a centrally arranged inner rod made of free-cutting steel with an outer diameter of 50 mm being provided in a casing tube according to Example 1 with an outer diameter of 210 mm and an inner diameter of 85 mm.
- the space was filled with a powder made of ledeburitic chrome steel.
- the casing tube was closed at its ends with sheet steel disks. Otherwise, the procedure was analogous to Example 1.
- an inner diameter of 212 mm and a length of 900 mm was a sleeve tube made of an alloy of the following composition in wt .-% C 0.45, Si 0.3 , Mn 0.7 and rest of iron with an outer diameter of 210 mm and an inner diameter of 85 mm and a length of 900 mm.
- a powder of the following composition in% by weight C 3.3, Cr 12.8, V 4, -5, Mo 1.1, W 1.0 and the rest iron was filled into this tube, a density of approx 65% was reached.
- Degassing was carried out at 370 ° C., whereupon an upper cover with a suction opening was welded onto the capsule tube. Then it was evacuated and the suction opening was closed.
- the encapsulated body was hot-isostatically pressed for 3 hours in an argon atmosphere at 1080 ° C. and a pressure of 1050 bar. This composite body was then forged on a long forging machine to an outer diameter of approximately 90 mm, which corresponds to a 5.4-fold deformation. After forging, heat treatment was carried out, after which an extruder cylinder was manufactured by mechanical processing and further heat treatment.
- Example 4 The procedure was analogous to Example 4, a powder of a cobalt-based alloy having the following composition in% by weight of C 0.25, Cr 8.25, Mo 5.5 and the rest of cobalt being used.
- an inner coating for example of Nik -. Kel or the like, which may occur as an adhesion promoter between the material of the sheath tube and the powder.
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Forging (AREA)
- Powder Metallurgy (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Glass Compositions (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
- Semiconductor Lasers (AREA)
- Manufacture And Refinement Of Metals (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
- Preventing Corrosion Or Incrustation Of Metals (AREA)
- Coating With Molten Metal (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT467982 | 1982-12-23 | ||
AT4679/82 | 1982-12-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0114593A1 true EP0114593A1 (de) | 1984-08-01 |
Family
ID=3567024
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP83890234A Withdrawn EP0114593A1 (de) | 1982-12-23 | 1983-12-22 | Verfahren zur Herstellung eines Maschinenhohlzylinders für Kunststoffverarbeitungsmaschinen |
EP83890232A Expired EP0114591B1 (de) | 1982-12-23 | 1983-12-22 | Verfahren zur Herstellung von Waffenrohren |
EP83890233A Expired EP0114592B1 (de) | 1982-12-23 | 1983-12-22 | Verfahren zur Metallverarbeitung unter Verwendung von Matrizen |
Family Applications After (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP83890232A Expired EP0114591B1 (de) | 1982-12-23 | 1983-12-22 | Verfahren zur Herstellung von Waffenrohren |
EP83890233A Expired EP0114592B1 (de) | 1982-12-23 | 1983-12-22 | Verfahren zur Metallverarbeitung unter Verwendung von Matrizen |
Country Status (6)
Country | Link |
---|---|
US (1) | US4747225A (enrdf_load_stackoverflow) |
EP (3) | EP0114593A1 (enrdf_load_stackoverflow) |
AT (2) | ATE33218T1 (enrdf_load_stackoverflow) |
DE (2) | DE3376100D1 (enrdf_load_stackoverflow) |
ES (2) | ES528317A0 (enrdf_load_stackoverflow) |
GR (2) | GR79748B (enrdf_load_stackoverflow) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0151103A3 (en) * | 1984-01-24 | 1988-01-20 | Vereinigte Edelstahlwerke Aktiengesellschaft (Vew) | Manufacturing method for elements of force, especially torque transmission |
AT391105B (de) * | 1988-10-07 | 1990-08-27 | Boehler Gmbh | Vormaterial fuer die erzeugung von verbundwerkstoffen |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4640814A (en) * | 1985-10-17 | 1987-02-03 | Crucible Materials Corporation | Method for producing clad tubular product |
DE3881923T2 (de) * | 1987-03-25 | 1994-01-27 | Nippon Steel Corp | Verfahren zur Herstellung von beschichteten Metallrohre. |
DE4136038C2 (de) * | 1990-11-02 | 1994-06-16 | Usui Kokusai Sangyo Kk | Geschweißtes Stahlrohr mit hoher Korrosionsbeständigkeit der Innenoberfläche sowie Verfahren zu seiner Herstellung |
US5290507A (en) * | 1991-02-19 | 1994-03-01 | Runkle Joseph C | Method for making tool steel with high thermal fatigue resistance |
US5341719A (en) * | 1992-12-14 | 1994-08-30 | General Electric Company | Multi-layer composite gun barrel |
US5357842A (en) * | 1993-07-09 | 1994-10-25 | Reynolds Charles E | Recoil reducing device |
US6218026B1 (en) | 1995-06-07 | 2001-04-17 | Allison Engine Company | Lightweight high stiffness member and manufacturing method thereof |
US5724643A (en) * | 1995-06-07 | 1998-03-03 | Allison Engine Company, Inc. | Lightweight high stiffness shaft and manufacturing method thereof |
US5856631A (en) * | 1995-11-20 | 1999-01-05 | Nitinol Technologies, Inc. | Gun barrel |
DE19834394A1 (de) * | 1998-07-30 | 2000-02-03 | Rheinmetall W & M Gmbh | Waffenrohr mit einer verschleißmindernden Hartchromschicht |
SE516130C2 (sv) * | 1999-03-15 | 2001-11-19 | Damasteel Ab | Ämne för metallprodukt, förfarande för framställning av metallprodukt samt metallprodukt |
RU2167742C2 (ru) * | 1999-03-31 | 2001-05-27 | Курский государственный технический университет | Способ армирования металлических изделий твердосплавным слоем |
DE19926246A1 (de) * | 1999-06-09 | 2000-12-14 | Rheinmetall W & M Gmbh | Verfahren zur Innenbeschichtung eines Waffenrohres |
US6594936B1 (en) * | 2002-10-03 | 2003-07-22 | Gary Sniezak | Method for lining a gun barrel |
US20040226211A1 (en) * | 2003-05-16 | 2004-11-18 | Ra Brands. L.L.C. | Composite receiver for firearms |
US20040244254A1 (en) * | 2003-06-09 | 2004-12-09 | Barfield Christopher A.. | Firearm safety device |
US7922065B2 (en) | 2004-08-02 | 2011-04-12 | Ati Properties, Inc. | Corrosion resistant fluid conducting parts, methods of making corrosion resistant fluid conducting parts and equipment and parts replacement methods utilizing corrosion resistant fluid conducting parts |
US7963202B1 (en) * | 2005-09-21 | 2011-06-21 | The United States Of America As Represented By The Secretary Of The Army | Superalloy mortar tube |
US7921590B2 (en) | 2006-02-23 | 2011-04-12 | Strum, Ruger & Company, Inc. | Composite firearm barrel reinforcement |
US20100236122A1 (en) * | 2006-07-26 | 2010-09-23 | Fonte Matthew V | Flowforming Gun Barrels and Similar Tubular Devices |
WO2008016353A1 (en) * | 2006-08-01 | 2008-02-07 | Afl Telecommunications Llc | Embedded metallic tubes with compression fit and method for manufacturing the same |
US8910409B1 (en) | 2010-02-09 | 2014-12-16 | Ati Properties, Inc. | System and method of producing autofrettage in tubular components using a flowforming process |
US8869443B2 (en) | 2011-03-02 | 2014-10-28 | Ati Properties, Inc. | Composite gun barrel with outer sleeve made from shape memory alloy to dampen firing vibrations |
US10118259B1 (en) | 2012-12-11 | 2018-11-06 | Ati Properties Llc | Corrosion resistant bimetallic tube manufactured by a two-step process |
US9279633B2 (en) | 2014-01-21 | 2016-03-08 | Richard R. Hayes | Multi-caliber weapon |
US9796057B2 (en) * | 2015-01-15 | 2017-10-24 | Saeilo Enterprises, Inc. | Gun barrel assembly |
SE2300011A1 (sv) * | 2023-02-09 | 2024-08-10 | Bae Systems Bofors Ab | Eldrör |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3753704A (en) * | 1967-04-14 | 1973-08-21 | Int Nickel Co | Production of clad metal articles |
DE2504032A1 (de) * | 1974-01-31 | 1975-08-07 | Nippon Musical Instruments Mfg | Verfahren zur herstellung von metallverbundstoffen |
DE2514565A1 (de) * | 1975-04-03 | 1976-10-14 | Uralsky Nii Trubnoj Promy | Verfahren zur herstellung von rohrerzeugnissen |
DE2855155A1 (de) * | 1977-12-22 | 1979-06-28 | United Technologies Corp | Verfahren zum herstellen eines fluidgekuehlten bedampfungstargets |
DE3114659A1 (de) * | 1980-04-10 | 1982-01-28 | Cameron Iron Works, Inc., Houston, Tex. | Verfahren zum auskleiden der hohlraeume in einem bauteil, beispielsweise einem ventil, sowie ausgekleidetes bauteil |
US4327154A (en) * | 1977-08-18 | 1982-04-27 | Motoren- Und Turbinen-Union Muenchen Gmbh | High-strength components of complex geometric shape and method for their manufacture |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US930927A (en) * | 1906-03-19 | 1909-08-10 | Robert H Berkstresser | Gun-barrel and process of producing the same. |
US2372202A (en) * | 1940-05-08 | 1945-03-27 | Mallory & Co Inc P R | Bearing |
US2636849A (en) * | 1946-12-13 | 1953-04-28 | Us Sec War | Method of electroforming gun barrels and liners |
US2977666A (en) * | 1954-12-29 | 1961-04-04 | Porter H Brace | Method of making gun liner elements |
US3112553A (en) * | 1960-06-08 | 1963-12-03 | William H Safranek | Electroforming of gun liners |
US3261121A (en) * | 1961-10-13 | 1966-07-19 | Joseph R Eves | Gun barrel with explosively welded liner |
US4016008A (en) * | 1975-07-31 | 1977-04-05 | The International Nickel Company, Inc. | Clad metal tubes |
US4426248A (en) * | 1983-05-20 | 1984-01-17 | The United States Of America As Represented By The Secretary Of The Army | Process for coating rifle tubes |
-
1983
- 1983-12-08 GR GR73197A patent/GR79748B/el unknown
- 1983-12-14 US US06/561,279 patent/US4747225A/en not_active Expired - Fee Related
- 1983-12-21 GR GR73306A patent/GR81355B/el unknown
- 1983-12-22 EP EP83890234A patent/EP0114593A1/de not_active Withdrawn
- 1983-12-22 EP EP83890232A patent/EP0114591B1/de not_active Expired
- 1983-12-22 AT AT83890232T patent/ATE33218T1/de not_active IP Right Cessation
- 1983-12-22 ES ES528317A patent/ES528317A0/es active Granted
- 1983-12-22 DE DE8383890232T patent/DE3376100D1/de not_active Expired
- 1983-12-22 AT AT83890233T patent/ATE33219T1/de not_active IP Right Cessation
- 1983-12-22 ES ES528315A patent/ES528315A0/es active Granted
- 1983-12-22 EP EP83890233A patent/EP0114592B1/de not_active Expired
- 1983-12-22 DE DE8383890233T patent/DE3376101D1/de not_active Expired
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3753704A (en) * | 1967-04-14 | 1973-08-21 | Int Nickel Co | Production of clad metal articles |
DE2504032A1 (de) * | 1974-01-31 | 1975-08-07 | Nippon Musical Instruments Mfg | Verfahren zur herstellung von metallverbundstoffen |
DE2514565A1 (de) * | 1975-04-03 | 1976-10-14 | Uralsky Nii Trubnoj Promy | Verfahren zur herstellung von rohrerzeugnissen |
US4327154A (en) * | 1977-08-18 | 1982-04-27 | Motoren- Und Turbinen-Union Muenchen Gmbh | High-strength components of complex geometric shape and method for their manufacture |
DE2855155A1 (de) * | 1977-12-22 | 1979-06-28 | United Technologies Corp | Verfahren zum herstellen eines fluidgekuehlten bedampfungstargets |
DE3114659A1 (de) * | 1980-04-10 | 1982-01-28 | Cameron Iron Works, Inc., Houston, Tex. | Verfahren zum auskleiden der hohlraeume in einem bauteil, beispielsweise einem ventil, sowie ausgekleidetes bauteil |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0151103A3 (en) * | 1984-01-24 | 1988-01-20 | Vereinigte Edelstahlwerke Aktiengesellschaft (Vew) | Manufacturing method for elements of force, especially torque transmission |
AT391105B (de) * | 1988-10-07 | 1990-08-27 | Boehler Gmbh | Vormaterial fuer die erzeugung von verbundwerkstoffen |
US5004653A (en) * | 1988-10-07 | 1991-04-02 | Boehler Ges. M.B.H. | Preliminary material for the production of composite material parts and method of making |
Also Published As
Publication number | Publication date |
---|---|
ES8501657A1 (es) | 1984-12-01 |
DE3376101D1 (en) | 1988-05-05 |
ES8501658A1 (es) | 1984-12-01 |
GR79748B (enrdf_load_stackoverflow) | 1984-10-31 |
ATE33218T1 (de) | 1988-04-15 |
EP0114591A1 (de) | 1984-08-01 |
ATE33219T1 (de) | 1988-04-15 |
ES528317A0 (es) | 1984-12-01 |
EP0114591B1 (de) | 1988-03-30 |
EP0114592A1 (de) | 1984-08-01 |
DE3376100D1 (en) | 1988-05-05 |
US4747225A (en) | 1988-05-31 |
EP0114592B1 (de) | 1988-03-30 |
ES528315A0 (es) | 1984-12-01 |
GR81355B (enrdf_load_stackoverflow) | 1984-12-11 |
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