US3418112A - Method for forming seamless pressure vessels - Google Patents
Method for forming seamless pressure vessels Download PDFInfo
- Publication number
- US3418112A US3418112A US584981A US58498166A US3418112A US 3418112 A US3418112 A US 3418112A US 584981 A US584981 A US 584981A US 58498166 A US58498166 A US 58498166A US 3418112 A US3418112 A US 3418112A
- Authority
- US
- United States
- Prior art keywords
- jacket
- article
- pressure
- sintered
- powders
- 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
- 238000000034 method Methods 0.000 title description 11
- 239000000463 material Substances 0.000 description 16
- 239000000843 powder Substances 0.000 description 16
- 238000004663 powder metallurgy Methods 0.000 description 10
- 239000000203 mixture Substances 0.000 description 9
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 238000003825 pressing Methods 0.000 description 7
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 6
- 229910052790 beryllium Inorganic materials 0.000 description 6
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 6
- 239000012530 fluid Substances 0.000 description 6
- 238000001953 recrystallisation Methods 0.000 description 6
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 5
- 238000007731 hot pressing Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000005245 sintering Methods 0.000 description 5
- 239000010936 titanium Substances 0.000 description 5
- 229910052719 titanium Inorganic materials 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 239000001307 helium Substances 0.000 description 4
- 229910052734 helium Inorganic materials 0.000 description 4
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 229910052786 argon Inorganic materials 0.000 description 3
- 238000005253 cladding Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 239000011733 molybdenum Substances 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 229910052721 tungsten Inorganic materials 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- LTPBRCUWZOMYOC-UHFFFAOYSA-N Beryllium oxide Chemical compound O=[Be] LTPBRCUWZOMYOC-UHFFFAOYSA-N 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000010962 carbon steel Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910000952 Be alloy Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
- 239000003870 refractory metal Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 229910001247 waspaloy Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 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
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
Definitions
- This invention relates in general to the fabrication of articles by powder metallurgy techniques and, more particularly, to the fabrication of seamless pressure vessels having containment walls characterized by a continuous, homogeneous, wrought microstructure.
- a further object is to provide a method for producing powder metallurgy articles having containment walls characterized by a homogeneous wrought microstructure.
- the desired pressure vessels or similar articles are produced by: isostatically pressing metal powders of the desired composition into the approximate configuration of the finished article and sintering the same to form a unitary body having a density approaching the calculated theoretical density; cladding the sintered body with a jacket of high relative strength; hot working the pressure vessel in compression against the jacket by the application of a fluid pressure against the unclad wall surface; and subsequently removing at least the major portion of the jacket from the worked pressure vessel.
- Satisfactory sintered bodies may be prepared by cold or warm pressing to the desired shape and, subsequently, subjecting the pressed powders to a sintering heat treatment.
- the powder metallurgy product is hot worked against a jacket or clad provided therearound.
- the jacket is applied to the article in any convenient manner and conforms in configuration to the surface of the article.
- the particular composition of the jacket is relatively unimportant but it will obviously possess the following properties: high strength relative to the article to be worked; thermal stability near or above the preferred hot working or recrystallization temperature of the material to be worked; preferably a different modulus of elasticity than the material to be worked; and chemical compatibility with the substrate.
- the clad is expandable tooling which will subsequently be discarded, one of the more common and inexpensive alloys meeting the previously discussed qualifications is normally used.
- one further factor may influence the selection of the cladding material. It is preferable in many cases to chemically etch the jacket from the pressure vessel upon completion of the hot working operation and, accordingly, when such an operation is contemplated the material may advantageously be selected on the basis of its susceptibility to the etching process. In any event, the jacket will provide a surface against which the powder metallurgy product may be hot worked at the preferred working parameters.
- the hot working operation is performed by applying a fluid pressure at the unclad wall surface of the vessel while it is held near or above the recrystallization temperature of the sintered material.
- an inert medium such as argon or helium is preferred as the pressurizing fluid.
- the particular working temperatures and pressures utilized to produce the desired Wrought microstructure will vary according to the particular powder composition initially used. While the usual practice will involve establishment of the preferred hot working parameters prior to the selection of a jacket material of suitable composition and strength to withstand the working pressures, there is considerable flexibility in the selection of these parameters. In any case, it is obvious that the characteristics of the clad will in some instances limit the pressures at which the sintered powders may be worked. Accordingly, drastic increases in the working pressure will necessarily be preceded by adjustments to the jacket material composition or thickness. Representative working parameters for several materials are set forth in Table II.
- Example I Pure beryllium powders were hot pressed into the shape of a pressure vessel having a diameter of approximately six inches with a wall thickness of 0.250 inch. Pressing was effected in a helium atmosphere at 1450 F., utilizing a pressure of 10,000 p.s.i.
- the powder metallurgy product was clad externally with a carbon steel jacket 0.75 inch thick, and pressurized internally with argon at 8000 p.s.i. while held at 1450 F.
- Metallurgical analysis revealed a wrought structure, and a yield strength increase from approximately 50,000 p.s.i. to 75,000 p.s.i. was noted.
- Example II Using a titanium base alloy of the nominal composition, by Weight, 13 percent vanadium, 11 percent chromium, 3 percent aluminum, balance titanium, the hot pressing parameters are 1500 F. at a pressure of 12,000 p.s.i. helium.
- a pressure vessel of the same size, wall thickness and configuration as that in Example I a Waspalloy (13.5 Co19.5 Cr4.25 Mo-1.25 Al3 Tibalance Ni) jacket of 0.5 inch thickness is utilized and the powders are worked at 10,000 p.s.i. in argon while held at 1750 F. to produce the desired wrought microstructure and a yield strength increase from 120,000 p.s.i. to approximately 180,000 p.s.i.
- Example III Using a fine grain beryllium alloy powder, designated I 400 and having the nominal composition, by weight, 4.25 percent beryllia, .2 percent aluminum, .5 percent carbon, .3 percent iron, .1 percent magnesium, .15 percent silicon, balance beryllium, the hot pressing parameters are 1450 F. and 20,000 p.s.i. helium. Hot working at 15,000 p.s.i. and 1450 F. with inert gas against a carbon steel jacket of 0.75 inch thickness produces a wrought microstructure and a yield strength increase from 70,000 p.s.i. to approximately 120,000 p.s.i.
- pressure vessels are produced in a wide variety of shapes having optimum strength characteristics. Further, since there are no wall discontinuities, such as those arising from changes in microstructure at weld areas in more conventional articles, the reliability of such articles in the performance of their designed function is much increased.
- the sintered article cladding the sintered article to provide an exterior jacket therearound against which the sintered powders may be hot worked, the jacket at the recrystallization temperature of the sintered powders having a strength exceeding that of the sintered article and a modulus of elasticity less than that of the sintered article,
- metal powders consist of as their principal component at least one metal selected from the group consisting of beryllium, titanium, aluminum, molybdenum and tungsten.
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Powder Metallurgy (AREA)
Description
United Smtes Patent ABSTRACT OF THE DISCLOSURE Powders of metals such as beryllium, titanium, aluminum, molybdenum and tungsten are pressed and sintered to form a fully dense, powder metallurgy article which is subsequently deformed against a jacket in a hot working operation utilizing a fluid pressure applied to the unclad surface of the articles.
This invention relates in general to the fabrication of articles by powder metallurgy techniques and, more particularly, to the fabrication of seamless pressure vessels having containment walls characterized by a continuous, homogeneous, wrought microstructure.
Many of the high strength metals and alloys possess physical properties which would make their use attractive as the materials of construction for space age pressure vessels and similar hardware. Unfortunately, however, many of these materials are diflicult to fabricate by conventional methods and are, furthermore, susceptible to such physical phenomena such as localized embrittlement in or adjacent weld areas used to join one detail to another. As a consequence, articles formed of these materials have not enjoyed the wide utility or approached the potential which their theoretical capabilities would suggest, particularly in high stressed components such as pressure vessels.
Depending, of course, upon the particular ultimate application in mind and the environment to which the article is to be exposed, hardware of the nature hereinbefore discussed has been constructed at various times from beryllium, zirconium, titanium, the refractory metals including molybdenum and tungsten, and the dispersion strengthened nickel and aluminum alloys. While various fabrication techniques have been utilized, the powder metallurgy approach has shown particular promise, particularly in the manufacture of articles of irregular shape.
It is an object of the present invention to provide an improved method for fabricating seamless pressure vessels of high strength by powder metallurgy techniques.
A further object is to provide a method for producing powder metallurgy articles having containment walls characterized by a homogeneous wrought microstructure.
These and other objects and advantages will be discussed in the detailed description which follows or will be evident therefrom or from practice of the invention.
According to the present invention and briefly stated, the desired pressure vessels or similar articles are produced by: isostatically pressing metal powders of the desired composition into the approximate configuration of the finished article and sintering the same to form a unitary body having a density approaching the calculated theoretical density; cladding the sintered body with a jacket of high relative strength; hot working the pressure vessel in compression against the jacket by the application of a fluid pressure against the unclad wall surface; and subsequently removing at least the major portion of the jacket from the worked pressure vessel.
In connection with the initial pressing operation wherein the powders are first compacted, it will usually be found preferable to apply the requisite pressure to the powders Patented Dec. 24, 1968 'ice while they are held at a temperature near or above their sintering temperature in a hot pressing operation. In general, the simultaneous application of temperature and pressure will provide an article of the highest density and, usually, a fully dense article. The particular preferred pressures and temperatures used at this stage of the process will, of course, vary depending upon the particular composition of the materials, as will he recognized by those skilled in the art, and the sintering temperature will vary somewhat as an inverse function of the applied pressure. In any event, the temperature-pressure selection will be such as to yield a fully dense, sintered compact upon completion of the hot pressing operation. The particularly preferred pressing parameters for a number of suitable high strength materials are set forth in Table I.
TABLE I Material Temperature F.) Pressure (p.s.i.)
The simultaneous application of temperature and pressure in the pressing operation may not, in certain circumstances, be convenient or even feasible, due usually to equipment limitations. In such cases, the pressing and sintering phases will necessarily have to be performed sequentially. Satisfactory sintered bodies may be prepared by cold or warm pressing to the desired shape and, subsequently, subjecting the pressed powders to a sintering heat treatment.
In order to take full advantage of the strength increases associated with a wrought metallurgical grain structure, the powder metallurgy product is hot worked against a jacket or clad provided therearound. The jacket is applied to the article in any convenient manner and conforms in configuration to the surface of the article. The particular composition of the jacket is relatively unimportant but it will obviously possess the following properties: high strength relative to the article to be worked; thermal stability near or above the preferred hot working or recrystallization temperature of the material to be worked; preferably a different modulus of elasticity than the material to be worked; and chemical compatibility with the substrate. For the sake of economy, since the clad is expandable tooling which will subsequently be discarded, one of the more common and inexpensive alloys meeting the previously discussed qualifications is normally used. In some instances one further factor may influence the selection of the cladding material. It is preferable in many cases to chemically etch the jacket from the pressure vessel upon completion of the hot working operation and, accordingly, when such an operation is contemplated the material may advantageously be selected on the basis of its susceptibility to the etching process. In any event, the jacket will provide a surface against which the powder metallurgy product may be hot worked at the preferred working parameters.
The hot working operation is performed by applying a fluid pressure at the unclad wall surface of the vessel while it is held near or above the recrystallization temperature of the sintered material. To prevent contamination in the working operation, an inert medium such as argon or helium is preferred as the pressurizing fluid. The particular working temperatures and pressures utilized to produce the desired Wrought microstructure will vary according to the particular powder composition initially used. While the usual practice will involve establishment of the preferred hot working parameters prior to the selection of a jacket material of suitable composition and strength to withstand the working pressures, there is considerable flexibility in the selection of these parameters. In any case, it is obvious that the characteristics of the clad will in some instances limit the pressures at which the sintered powders may be worked. Accordingly, drastic increases in the working pressure will necessarily be preceded by adjustments to the jacket material composition or thickness. Representative working parameters for several materials are set forth in Table II.
TABLE II Material Temperature F.) Pressure (p.s.i.)
Example I Pure beryllium powders were hot pressed into the shape of a pressure vessel having a diameter of approximately six inches with a wall thickness of 0.250 inch. Pressing was effected in a helium atmosphere at 1450 F., utilizing a pressure of 10,000 p.s.i. The powder metallurgy product Was clad externally with a carbon steel jacket 0.75 inch thick, and pressurized internally with argon at 8000 p.s.i. while held at 1450 F.
Metallurgical analysis revealed a wrought structure, and a yield strength increase from approximately 50,000 p.s.i. to 75,000 p.s.i. was noted.
Example II Using a titanium base alloy of the nominal composition, by Weight, 13 percent vanadium, 11 percent chromium, 3 percent aluminum, balance titanium, the hot pressing parameters are 1500 F. at a pressure of 12,000 p.s.i. helium. For a pressure vessel of the same size, wall thickness and configuration as that in Example I, a Waspalloy (13.5 Co19.5 Cr4.25 Mo-1.25 Al3 Tibalance Ni) jacket of 0.5 inch thickness is utilized and the powders are worked at 10,000 p.s.i. in argon while held at 1750 F. to produce the desired wrought microstructure and a yield strength increase from 120,000 p.s.i. to approximately 180,000 p.s.i.
Example III Using a fine grain beryllium alloy powder, designated I 400 and having the nominal composition, by weight, 4.25 percent beryllia, .2 percent aluminum, .5 percent carbon, .3 percent iron, .1 percent magnesium, .15 percent silicon, balance beryllium, the hot pressing parameters are 1450 F. and 20,000 p.s.i. helium. Hot working at 15,000 p.s.i. and 1450 F. with inert gas against a carbon steel jacket of 0.75 inch thickness produces a wrought microstructure and a yield strength increase from 70,000 p.s.i. to approximately 120,000 p.s.i.
As may readily be seen, through the techniques taught in the present invention, pressure vessels are produced in a wide variety of shapes having optimum strength characteristics. Further, since there are no wall discontinuities, such as those arising from changes in microstructure at weld areas in more conventional articles, the reliability of such articles in the performance of their designed function is much increased.
While the invention has been described in connection with several examples and specific material compositions, its applicability to other systems will be evident within strength exceeding that of the sintered article at its recrystallization temperature, heating the clad article to the recrystallization temperature of the sintered article and applying a fluid pressure to the unclad wall of the article to effect deformation thereof against the clad in a hot working operation, and removing the clad from the article. 2. The method of forming a seamless pressure vessel by powder metallurgy techniques comprising the steps of: hot pressing metal powders into the shape of a pressure vessel in an inert atmosphere to form a fully dense sintered article,
cladding the sintered article to provide an exterior jacket therearound against which the sintered powders may be hot worked, the jacket at the recrystallization temperature of the sintered powders having a strength exceeding that of the sintered article and a modulus of elasticity less than that of the sintered article,
heating the jacketed article to effect recrystallization of the sintered powders and internally pressurizing the jacketed article with an inert fluid to compressively work the sintered powders against the jacket,
and removing at least the major portion of the jacket from the worked pressure vessel.
3. The method of claim 2 wherein the metal powders consist of as their principal component at least one metal selected from the group consisting of beryllium, titanium, aluminum, molybdenum and tungsten.
References Cited UNITED STATES PATENTS 2,337,247 12/ 1943 Kepler.
2,752,669 7/1956 Carr 29-421 X 2,916,809 12/1959 Schell 45-226 X 3,114,968 12/1963 Rudelick 29-4205 3,127,671 4/ 1964 Hayes 29-423 3,135,045 6/1964 Schane 29-423 3,156,973 11/1964 Lieberman. 3,197,851 8/1965 Aleck 29421 3,242,563 3/ 1966 Turner 29-423 3,249,410 5/1966 Lorenzo 75-214 X 3,268,368 8/1966 Mackiw 75-214 X OTHER REFERENCES Beryllium Processing by Powder Metallurgy: by H. G. Wihle and V. C. Potter, August 1961, Journal of Metals, pp. 537538.
BENJAMIN R. PADGETT, Primary Examiner. A. J. STEINER, Assistant Examiner.
US. Cl. X.R.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US584981A US3418112A (en) | 1966-10-07 | 1966-10-07 | Method for forming seamless pressure vessels |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US584981A US3418112A (en) | 1966-10-07 | 1966-10-07 | Method for forming seamless pressure vessels |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3418112A true US3418112A (en) | 1968-12-24 |
Family
ID=24339557
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US584981A Expired - Lifetime US3418112A (en) | 1966-10-07 | 1966-10-07 | Method for forming seamless pressure vessels |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3418112A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3999986A (en) * | 1974-04-08 | 1976-12-28 | Lockheed Missiles & Space Company, Inc. | Method for making high ductility beryllium bodies |
| WO2010041957A1 (en) * | 2008-10-10 | 2010-04-15 | Tool-Tech As | Method for production of an acid proof, seemless pressure vessel |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2337247A (en) * | 1938-04-29 | 1943-12-21 | Smith Corp A O | Method of making multilayer vessels |
| US2752669A (en) * | 1953-09-29 | 1956-07-03 | Edward Valves Inc | Methods for manufacturing high pressure vessels |
| US2916809A (en) * | 1958-06-30 | 1959-12-15 | Donald H Schell | Tungsten base alloys |
| US3114968A (en) * | 1961-09-20 | 1963-12-24 | Bruner Corp | Method of making pressure vessels |
| US3127671A (en) * | 1961-06-27 | 1964-04-07 | Ladish Co | Art of forging brittle metals |
| US3135045A (en) * | 1961-04-19 | 1964-06-02 | Budd Co | Method for forming articles from thin sheet material |
| US3156973A (en) * | 1962-04-12 | 1964-11-17 | Aerojet General Co | Method of producing interior surface contour on tubular part by explosive forming |
| US3197851A (en) * | 1962-03-28 | 1965-08-03 | Arde Portland Inc | Method of forming a high tensile stength pressure vessel |
| US3242563A (en) * | 1961-12-06 | 1966-03-29 | Int Nickel Co | Plastic deformation of alloys |
| US3249410A (en) * | 1962-09-28 | 1966-05-03 | A P De Sanno & Son Inc | Process of making metal bonded diamond abrasive articles |
| US3268368A (en) * | 1963-10-21 | 1966-08-23 | Sherritt Gordon Mines Ltd | Process for the production of wrought nickel strip and sheet of low hardness |
-
1966
- 1966-10-07 US US584981A patent/US3418112A/en not_active Expired - Lifetime
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2337247A (en) * | 1938-04-29 | 1943-12-21 | Smith Corp A O | Method of making multilayer vessels |
| US2752669A (en) * | 1953-09-29 | 1956-07-03 | Edward Valves Inc | Methods for manufacturing high pressure vessels |
| US2916809A (en) * | 1958-06-30 | 1959-12-15 | Donald H Schell | Tungsten base alloys |
| US3135045A (en) * | 1961-04-19 | 1964-06-02 | Budd Co | Method for forming articles from thin sheet material |
| US3127671A (en) * | 1961-06-27 | 1964-04-07 | Ladish Co | Art of forging brittle metals |
| US3114968A (en) * | 1961-09-20 | 1963-12-24 | Bruner Corp | Method of making pressure vessels |
| US3242563A (en) * | 1961-12-06 | 1966-03-29 | Int Nickel Co | Plastic deformation of alloys |
| US3197851A (en) * | 1962-03-28 | 1965-08-03 | Arde Portland Inc | Method of forming a high tensile stength pressure vessel |
| US3156973A (en) * | 1962-04-12 | 1964-11-17 | Aerojet General Co | Method of producing interior surface contour on tubular part by explosive forming |
| US3249410A (en) * | 1962-09-28 | 1966-05-03 | A P De Sanno & Son Inc | Process of making metal bonded diamond abrasive articles |
| US3268368A (en) * | 1963-10-21 | 1966-08-23 | Sherritt Gordon Mines Ltd | Process for the production of wrought nickel strip and sheet of low hardness |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3999986A (en) * | 1974-04-08 | 1976-12-28 | Lockheed Missiles & Space Company, Inc. | Method for making high ductility beryllium bodies |
| WO2010041957A1 (en) * | 2008-10-10 | 2010-04-15 | Tool-Tech As | Method for production of an acid proof, seemless pressure vessel |
| US20110215510A1 (en) * | 2008-10-10 | 2011-09-08 | Egil Eriksen | Method for production of an acid proof, seemless pressure vessel |
| AU2009302974B2 (en) * | 2008-10-10 | 2013-01-24 | Tool-Tech As | Method for production of an acid proof, seemless pressure vessel |
| US8894913B2 (en) | 2008-10-10 | 2014-11-25 | Tool-Tech As | Method for production of an acid proof, seemless pressure vessel |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Igharo et al. | Compaction and sintering phenomena in titanium—nickel shape memory alloys | |
| US5190603A (en) | Process for producing a workpiece from an alloy containing dopant and based on titanium aluminide | |
| US4752335A (en) | Process for the manufacture of a target for cathodic sputtering | |
| US3999952A (en) | Sintered hard alloy of multiple boride containing iron | |
| JPS58151242A (en) | Material with two-way memory effect that causes reversible shape change due to thermal change and method for producing the same | |
| US3639179A (en) | Method of making large grain-sized superalloys | |
| US5788142A (en) | Process for joining, coating or repairing parts made of intermetallic material | |
| US5424027A (en) | Method to produce hot-worked gamma titanium aluminide articles | |
| JPH0328965B2 (en) | ||
| US3698962A (en) | Method for producing superalloy articles by hot isostatic pressing | |
| US3672881A (en) | Method of making powder composites | |
| Hodge | Elevated-temperature compaction of metals and ceramics by gas pressures | |
| US4410488A (en) | Powder metallurgical process for producing a copper-based shape-memory alloy | |
| US3418112A (en) | Method for forming seamless pressure vessels | |
| US3700434A (en) | Titanium-nickel alloy manufacturing methods | |
| US4534808A (en) | Method for refining microstructures of prealloyed powder metallurgy titanium articles | |
| US4428778A (en) | Process for producing metallic chromium plates and sheets | |
| US3243291A (en) | High-temperature alloy | |
| US2973570A (en) | High temperature structural material and method of producing same | |
| US3301671A (en) | Aluminous sintered parts and techniques for fabricating same | |
| US4808225A (en) | Method for producing an alloy product of improved ductility from metal powder | |
| US2228600A (en) | Powder metallurgy | |
| US3724050A (en) | Method of making beryllium shapes from powder metal | |
| US2947068A (en) | Aluminum base powder products | |
| US3672037A (en) | Nitride strengthened stainless steel composite and production thereof |