WO1996033831A1 - Method of manufacturing high temperature resistant shaped parts - Google Patents
Method of manufacturing high temperature resistant shaped parts Download PDFInfo
- Publication number
- WO1996033831A1 WO1996033831A1 PCT/SE1996/000535 SE9600535W WO9633831A1 WO 1996033831 A1 WO1996033831 A1 WO 1996033831A1 SE 9600535 W SE9600535 W SE 9600535W WO 9633831 A1 WO9633831 A1 WO 9633831A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- high temperature
- shaped parts
- temperature resistant
- manufacturing high
- weight
- Prior art date
Links
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
- B22F3/14—Both compacting and sintering simultaneously
- B22F3/15—Hot isostatic pressing
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/08—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
- C23C8/10—Oxidising
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
- C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
- C22C33/0285—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with Cr, Co, or Ni having a minimum content higher than 5%
Definitions
- the present invention is for a method of manufacturing high temperature resistant shaped parts made of metal alloy.
- Metallic alloys can, when properly selected with regard to alloy composition, be used at high temperatures.
- High temperature is in this respect considered to be 1100°C and higher.
- Alloys of iron-chromium-aluminium, i.e. FeCrAl alloys can be used at temperatures as high as 1200-1400°C and also somewhat higher temperatures.
- Such alloys have the advantage of being extremely resistant to oxidizing and corrosive environments at high temperatures.
- the use of these alloys has been restricted due to difficulties in shaping parts of more intricate design.
- the method according to the present invention makes it possible to manufacture shaped parts of a high temperature FeCrAl alloy.
- Shaped parts are considered to be parts and products which are not in the shape of rod, strip tubes or similar which can be produced by means of extrusion of billets. Shaped parts are for example muffles, tubes, bends, crucibles and burner dies of complicated shape.
- the invention also comprises a suitable starting material for use in the invented method.
- high temperature resistant shaped parts of FeCrAl alloy are produced from metal powder of desired composition by means of hot isostatic pressing to a predetermined shape in a metal container.
- the alloy preferrably contains 2-10 weight-% aluminium, 10-40 weight-% chromium, balance basically iron.
- the alloy can also hold small amounts of for example cobalt, nickel, silicon, manganese, zirconium, titanium, yttrium, vanadium, tantalum and rare earth metals.
- the present invention also includes alloys with such additions.
- the powder used in accordance with the way of production of the invention is produced by atomization of molten metal by known methods.
- the powder is put into a metal container which can be shaped in such a way as to produce a part which upon hot isostatic pressing is given a shape which is ready for use.
- the container material is removed by chemical or mechanical means, for example pickling or turning.
- Another way to produce a powder metallurgical part of finished shape for hot isostatic pressing is metal injection moulding (MIM), in which process a mixture of metal powder and a binder is shaped into a green body. The green body is sintered and the binder is burnt off.
- MIM metal injection moulding
- the surface of the component is preoxidized prior to use. In doing so, a layer of aluminium oxide is formed on the surface. This is also the case under normal operating conditions, when this is done at high temperature and in oxidizing atmosphere. By preoxidation the properties of the layer can be better controlled and more dense layer can be obtained than would otherwise be the case. Also in non-oxidizing atmosphere such a layer has good heat resistance. Products manufactured as described in the invention have unique properties in aggressive enviroments, especially in carbon and sulphur containing atmospheres.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacturing & Machinery (AREA)
- Powder Metallurgy (AREA)
- Glass Compositions (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU55208/96A AU696386B2 (en) | 1995-04-26 | 1996-04-23 | Method of manufacturing high temperature resistant shaped parts |
JP53243296A JP4384727B2 (en) | 1995-04-26 | 1996-04-23 | Manufacturing method of heat-resistant molded parts |
DE69617668T DE69617668T2 (en) | 1995-04-26 | 1996-04-23 | METHOD FOR PRODUCING HIGH TEMPERATURE RESISTANT MOLDED PARTS |
EP96912376A EP0822875B1 (en) | 1995-04-26 | 1996-04-23 | Method of manufacturing high temperature resistant shaped parts |
NO974177A NO974177L (en) | 1995-04-26 | 1997-09-10 | Process for producing high temperature resistant molded parts |
US08/943,937 US5970306A (en) | 1995-04-26 | 1997-09-30 | Method of manufacturing high temperature resistant shaped parts |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9501534 | 1995-04-26 | ||
SE9501534A SE504208C2 (en) | 1995-04-26 | 1995-04-26 | Method of manufacturing high temperature resistant moldings |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US08/943,937 Continuation US5970306A (en) | 1995-04-26 | 1997-09-30 | Method of manufacturing high temperature resistant shaped parts |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1996033831A1 true WO1996033831A1 (en) | 1996-10-31 |
Family
ID=20398090
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/SE1996/000535 WO1996033831A1 (en) | 1995-04-26 | 1996-04-23 | Method of manufacturing high temperature resistant shaped parts |
Country Status (10)
Country | Link |
---|---|
US (1) | US5970306A (en) |
EP (1) | EP0822875B1 (en) |
JP (1) | JP4384727B2 (en) |
KR (1) | KR100425872B1 (en) |
AU (1) | AU696386B2 (en) |
DE (1) | DE69617668T2 (en) |
ES (1) | ES2169239T3 (en) |
NO (1) | NO974177L (en) |
SE (1) | SE504208C2 (en) |
WO (1) | WO1996033831A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1999026019A1 (en) * | 1997-11-18 | 1999-05-27 | J. Eberspächer Gmbh & Co. | Method for producing a combustion chamber, and combustion chamber of a vehicle heating device, produced according to this method |
WO1999040231A1 (en) * | 1998-02-04 | 1999-08-12 | Sandvik Ab; (Publ) | Dispersion hardening alloy and method for the production of the alloy |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE521670C2 (en) * | 1999-05-27 | 2003-11-25 | Sandvik Ab | Heat and oxidation resistant metallic material containing aluminum comprises silicon and/or silicon-containing compound(s) applied onto its surface |
EP2051826B1 (en) * | 2006-07-21 | 2011-09-21 | Höganäs Aktiebolag | Iron-based powder |
US20120034101A1 (en) * | 2010-08-09 | 2012-02-09 | James Allister W | Turbine blade squealer tip |
CN113305288B (en) * | 2021-05-28 | 2023-07-25 | 江苏智林空间装备科技有限公司 | Fe-Cr-Al-Cu-Ni alloy for tail gas purifying device of military diesel vehicle and preparation method thereof |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3293007A (en) * | 1965-11-29 | 1966-12-20 | Carl S Wukusick | Steam corrosion-resistant iron-chromium-aluminum-yttrium alloys and process for making same |
US3964877A (en) * | 1975-08-22 | 1976-06-22 | General Electric Company | Porous high temperature seal abradable member |
US4023966A (en) * | 1975-11-06 | 1977-05-17 | United Technologies Corporation | Method of hot isostatic compaction |
US4077109A (en) * | 1976-05-10 | 1978-03-07 | The International Nickel Company, Inc. | Hot working of metal powders |
US4443249A (en) * | 1982-03-04 | 1984-04-17 | Huntington Alloys Inc. | Production of mechanically alloyed powder |
US4427447A (en) * | 1982-03-31 | 1984-01-24 | Exxon Research And Engineering Co. | Alumina-yttria mixed oxides in dispersion strengthened high temperature alloy powders |
US4647304A (en) * | 1983-08-17 | 1987-03-03 | Exxon Research And Engineering Company | Method for producing dispersion strengthened metal powders |
US5427601A (en) * | 1990-11-29 | 1995-06-27 | Ngk Insulators, Ltd. | Sintered metal bodies and manufacturing method therefor |
JPH04308065A (en) * | 1991-04-04 | 1992-10-30 | Daido Steel Co Ltd | Material having high electric resistance and production thereof |
JPH04308064A (en) * | 1991-04-04 | 1992-10-30 | Daido Steel Co Ltd | Material having high electric resistance and production thereof |
-
1995
- 1995-04-26 SE SE9501534A patent/SE504208C2/en not_active IP Right Cessation
-
1996
- 1996-04-23 AU AU55208/96A patent/AU696386B2/en not_active Ceased
- 1996-04-23 KR KR1019970707500A patent/KR100425872B1/en not_active IP Right Cessation
- 1996-04-23 JP JP53243296A patent/JP4384727B2/en not_active Expired - Fee Related
- 1996-04-23 ES ES96912376T patent/ES2169239T3/en not_active Expired - Lifetime
- 1996-04-23 WO PCT/SE1996/000535 patent/WO1996033831A1/en active IP Right Grant
- 1996-04-23 DE DE69617668T patent/DE69617668T2/en not_active Expired - Lifetime
- 1996-04-23 EP EP96912376A patent/EP0822875B1/en not_active Expired - Lifetime
-
1997
- 1997-09-10 NO NO974177A patent/NO974177L/en not_active Application Discontinuation
- 1997-09-30 US US08/943,937 patent/US5970306A/en not_active Expired - Lifetime
Non-Patent Citations (3)
Title |
---|
DIALOG INFORMATION SERVICES, File 351, World Patent Index 81-96, WPI Accession No. 92-411329/50, DAIDO TOKUSHUKO KK, "High Electrical Resistance as Heating Iron-Chromium-Aluminium Alloy Conditions, Prepd. by Hot Compression Moulding Powder"; & JP,A,04 308 064, (30-10-92), 9250, (BASIC). * |
DIALOG INFORMATION SERVICES, File 351, World Patent Index 81-96, WPI Accession No. 92-411330/50, DAIDO TOKUSHUKO KK, "High Electric Resistance Iron-Chromium-Aluminium Alloy-Comprises Container, Useful as Support Catalyst for Automobile Exhaust Gas Treatment"; & JP,A,04 308 065, (30-10-92), 9250, (BASIC). * |
PATENT ABSTRACTS OF JAPAN, Vol. 17, No. 345, C-1077; & JP,A,05 043 976, (KOBE STEEL LTD et al.), 23 February 1993. * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1999026019A1 (en) * | 1997-11-18 | 1999-05-27 | J. Eberspächer Gmbh & Co. | Method for producing a combustion chamber, and combustion chamber of a vehicle heating device, produced according to this method |
WO1999040231A1 (en) * | 1998-02-04 | 1999-08-12 | Sandvik Ab; (Publ) | Dispersion hardening alloy and method for the production of the alloy |
US6231807B1 (en) | 1998-02-04 | 2001-05-15 | Sandvik Ab | Dispersion hardening alloy and method for the production of the alloy |
Also Published As
Publication number | Publication date |
---|---|
AU696386B2 (en) | 1998-09-10 |
EP0822875A1 (en) | 1998-02-11 |
NO974177D0 (en) | 1997-09-10 |
SE9501534D0 (en) | 1995-04-26 |
JP4384727B2 (en) | 2009-12-16 |
SE504208C2 (en) | 1996-12-09 |
KR100425872B1 (en) | 2004-06-12 |
US5970306A (en) | 1999-10-19 |
ES2169239T3 (en) | 2002-07-01 |
EP0822875B1 (en) | 2001-12-05 |
DE69617668D1 (en) | 2002-01-17 |
KR19990007976A (en) | 1999-01-25 |
SE9501534L (en) | 1996-10-27 |
DE69617668T2 (en) | 2002-08-14 |
NO974177L (en) | 1997-09-10 |
JPH11504078A (en) | 1999-04-06 |
AU5520896A (en) | 1996-11-18 |
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