GB934542A - Protective coating on refractory metals - Google Patents
Protective coating on refractory metalsInfo
- Publication number
- GB934542A GB934542A GB1824/62A GB182462A GB934542A GB 934542 A GB934542 A GB 934542A GB 1824/62 A GB1824/62 A GB 1824/62A GB 182462 A GB182462 A GB 182462A GB 934542 A GB934542 A GB 934542A
- Authority
- GB
- United Kingdom
- Prior art keywords
- boron
- silicon
- source
- inert diluent
- metal
- 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
Links
Classifications
-
- 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
- C23C12/00—Solid state diffusion of at least one non-metal element other than silicon and at least one metal element or silicon into metallic material surfaces
- C23C12/02—Diffusion in one step
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/02—Surface coverings of combustion-gas-swept parts
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/938—Vapor deposition or gas diffusion
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/941—Solid state alloying, e.g. diffusion, to disappearance of an original layer
-
- 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
- Y10T428/12139—Nonmetal particles in particulate component
-
- 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
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12806—Refractory [Group IVB, VB, or VIB] metal-base component
- Y10T428/12812—Diverse refractory group metal-base components: alternative to or next to each other
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Combustion & Propulsion (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
- Powder Metallurgy (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Chemically Coating (AREA)
Abstract
A base metal of the group consisting of molybdenum, tantalum, tungsten, niobium, and alloys thereof including other metals such as 0.5% titanium or zirconium, is heated in a non-oxidizing atmosphere in contact with a powdered mixture containing an inert diluent, a silicon and boron source and a halogen source, to diffuse silicon and boron into the surface of the base metal to form a continuous protective coating rendering the metal resistant to oxidation in such parts as nozzles, blades, vanes and shells which are required to operate in air at 1800 DEG to 3600 DEG F. The silicon and boron, which may be elemental and powdered to 60-325 mesh (Tyler) size or of other source such as ferro-silicon and ferro-boron, are preferably heated and alloyed together. Both alloying and diffusion may occur at 1600 DEG to 2200 DEG F. The inert diluent may be a refractory material of grain size 50-350 mesh (Tyler), e.g. clay, kaolin, zirconia, beryllia, alumina. The halogen source may be fluorine, chlorine, bromine or iodine, or metal or ammonium halides, preferably ammonium bifluoride. An example of a diffusion pack composition by weight is: Si 5-70%, B 1/8 -10%, halogen source 0.1-1%, inert diluent 25-75%. A molybdenum alloy containing 0.5% Ti and 0.07% Zr is specified.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US83953A US3090702A (en) | 1961-01-23 | 1961-01-23 | Protective coating of refractory metals |
Publications (1)
Publication Number | Publication Date |
---|---|
GB934542A true GB934542A (en) | 1963-08-21 |
Family
ID=22181727
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1824/62A Expired GB934542A (en) | 1961-01-23 | 1962-01-18 | Protective coating on refractory metals |
Country Status (3)
Country | Link |
---|---|
US (1) | US3090702A (en) |
DE (1) | DE1446118B2 (en) |
GB (1) | GB934542A (en) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3307964A (en) * | 1963-05-07 | 1967-03-07 | Du Pont | Process of forming protective coatings on columbium and tantalum using a fluidized bed |
DE1496176C3 (en) * | 1964-06-12 | 1975-02-27 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Catalysts for fuel electrodes of fuel elements with acidic electrolytes |
US3409459A (en) * | 1965-03-10 | 1968-11-05 | Du Pont | Fluidized bed coating of titaniumchromium alloy |
US3442720A (en) * | 1965-10-23 | 1969-05-06 | United Aircraft Corp | Method of forming ti-modified silicide coatings on cb-base substrates and resulting articles |
US3455745A (en) * | 1966-07-08 | 1969-07-15 | Dow Corning | Coating of objects with tetraboron silicide |
US3607367A (en) * | 1968-04-01 | 1971-09-21 | Gen Technologies Corp | High-strength, high-modulus, low density, boron silicide monofilaments, and method of making same |
US3622374A (en) * | 1969-01-14 | 1971-11-23 | Ritter Praulder Corp | Diffusion coating of ferrous articles |
US3787245A (en) * | 1970-10-26 | 1974-01-22 | Inst Haertereitechn | Method for the boration of titanium and titanium alloys |
US3936327A (en) * | 1972-09-07 | 1976-02-03 | Elektroschmelzwerk Kempten Gmbh | Boriding composition |
US3859144A (en) * | 1973-06-27 | 1975-01-07 | United Aircraft Corp | Method for producing nickel alloy bonding foil |
US5455068A (en) * | 1994-04-28 | 1995-10-03 | Aves, Jr.; William L. | Method for treating continuous extended lengths of tubular member interiors |
US5613299A (en) * | 1994-11-09 | 1997-03-25 | Ring; Peter J. | Method of fabricating a rocket thrust chamber |
GB9915430D0 (en) | 1999-07-01 | 1999-09-01 | Artemis Intelligent Power Limi | A heat engine system |
US6340398B1 (en) * | 2000-04-04 | 2002-01-22 | The United States Of America As Represented By The Secretary Of The Air Force | Oxidation protective coating for Mo-Si-B alloys |
US7005191B2 (en) * | 2003-05-01 | 2006-02-28 | Wisconsin Alumni Research Foundation | Oxidation resistant coatings for ultra high temperature transition metals and transition metal alloys |
US8316679B2 (en) | 2010-10-04 | 2012-11-27 | Siemens Industry, Inc. | Boronized laying pipe |
CN109972081A (en) * | 2019-05-05 | 2019-07-05 | 中国人民解放军空军工程大学 | A kind of molybdenum silicon boron powder for metal part surface infiltration layer and preparation method thereof and infiltration layer preparation method |
CN110863172A (en) * | 2019-11-16 | 2020-03-06 | 北方民族大学 | Cr-Si-Zr-B permeating agent and application method thereof on tantalum and tantalum alloy surface |
CN116397228B (en) * | 2023-06-06 | 2023-08-22 | 中南大学 | Method for preparing alloy/tantalum carbide composite coating on graphite surface |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2924004A (en) * | 1960-02-09 | Refractory metal bodies | ||
GB191219461A (en) * | 1912-08-24 | 1913-08-21 | Giulio Sirovich | Improvements in or relating to the Cementation of Metals. |
US2665998A (en) * | 1950-03-18 | 1954-01-12 | Fansteel Metallurgical Corp | Method of preparing highly refractory bodies |
US2865088A (en) * | 1952-10-16 | 1958-12-23 | Fansteel Metallurgical Corp | Refractory metal bodies |
US2811466A (en) * | 1953-03-18 | 1957-10-29 | Metal Diffusions Inc | Process of chromizing |
US2887420A (en) * | 1956-04-06 | 1959-05-19 | Bristol Aero Engines Ltd | Surface treatments for articles made from heat resisting alloys |
US2920006A (en) * | 1957-12-13 | 1960-01-05 | Leonard F Yntema | Highly refractive molybdenum bodies and method of preparing same |
-
1961
- 1961-01-23 US US83953A patent/US3090702A/en not_active Expired - Lifetime
-
1962
- 1962-01-18 GB GB1824/62A patent/GB934542A/en not_active Expired
- 1962-01-22 DE DE19621446118 patent/DE1446118B2/en active Pending
Also Published As
Publication number | Publication date |
---|---|
DE1446118A1 (en) | 1969-03-20 |
DE1446118B2 (en) | 1970-12-10 |
US3090702A (en) | 1963-05-21 |
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