GB1156721A - Improvements in and relating to Cast Metal Part and apparatus therefor - Google Patents
Improvements in and relating to Cast Metal Part and apparatus thereforInfo
- Publication number
- GB1156721A GB1156721A GB20371/66A GB2037166A GB1156721A GB 1156721 A GB1156721 A GB 1156721A GB 20371/66 A GB20371/66 A GB 20371/66A GB 2037166 A GB2037166 A GB 2037166A GB 1156721 A GB1156721 A GB 1156721A
- Authority
- GB
- United Kingdom
- Prior art keywords
- mould
- carried out
- blade
- nickel
- casting
- 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
- 239000002184 metal Substances 0.000 title 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 abstract 6
- 239000013078 crystal Substances 0.000 abstract 4
- 238000005266 casting Methods 0.000 abstract 3
- 229910052759 nickel Inorganic materials 0.000 abstract 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 abstract 2
- 229910045601 alloy Inorganic materials 0.000 abstract 2
- 239000000956 alloy Substances 0.000 abstract 2
- 238000010438 heat treatment Methods 0.000 abstract 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract 1
- 229910052786 argon Inorganic materials 0.000 abstract 1
- 229910002804 graphite Inorganic materials 0.000 abstract 1
- 239000010439 graphite Substances 0.000 abstract 1
- 239000012535 impurity Substances 0.000 abstract 1
- 230000006698 induction Effects 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 229910052750 molybdenum Inorganic materials 0.000 abstract 1
- 229910052758 niobium Inorganic materials 0.000 abstract 1
- 239000011253 protective coating Substances 0.000 abstract 1
- 238000007711 solidification Methods 0.000 abstract 1
- 230000008023 solidification Effects 0.000 abstract 1
- 229910000601 superalloy Inorganic materials 0.000 abstract 1
- 229910052721 tungsten Inorganic materials 0.000 abstract 1
- 229910052720 vanadium Inorganic materials 0.000 abstract 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B11/00—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
- C30B11/14—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method characterised by the seed, e.g. its crystallographic orientation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
- B22D27/04—Influencing the temperature of the metal, e.g. by heating or cooling the mould
- B22D27/045—Directionally solidified castings
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
-
- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B11/00—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
-
- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B29/00—Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
- C30B29/10—Inorganic compounds or compositions
- C30B29/52—Alloys
-
- 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
- Y10S117/00—Single-crystal, oriented-crystal, and epitaxy growth processes; non-coating apparatus therefor
- Y10S117/901—Levitation, reduced gravity, microgravity, space
- Y10S117/902—Specified orientation, shape, crystallography, or size of seed or substrate
-
- 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
- Y10S415/00—Rotary kinetic fluid motors or pumps
- Y10S415/915—Pump or portion thereof by casting or molding
-
- 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
- Y10T428/12375—All metal or with adjacent metals having member which crosses the plane of another member [e.g., T or X cross section, etc.]
-
- 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
- Y10T428/12389—All metal or with adjacent metals having variation in thickness
- Y10T428/12403—Longitudinally smooth and symmetrical
-
- 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
- Y10T428/12465—All metal or with adjacent metals having magnetic properties, or preformed fiber orientation coordinate with shape
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US45939165A | 1965-05-27 | 1965-05-27 | |
US54011466A | 1966-02-17 | 1966-02-17 | |
US76417168A | 1968-10-01 | 1968-10-01 | |
US87977269A | 1969-11-25 | 1969-11-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1156721A true GB1156721A (en) | 1969-07-02 |
Family
ID=27504055
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB20371/66A Expired GB1156721A (en) | 1965-05-27 | 1966-05-09 | Improvements in and relating to Cast Metal Part and apparatus therefor |
Country Status (8)
Country | Link |
---|---|
US (3) | US3494709A (forum.php) |
JP (1) | JPS501455B1 (forum.php) |
BE (1) | BE681776A (forum.php) |
CH (1) | CH489274A (forum.php) |
DE (2) | DE1533473B1 (forum.php) |
GB (1) | GB1156721A (forum.php) |
NL (1) | NL147046B (forum.php) |
SE (1) | SE330235B (forum.php) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2436254A1 (fr) * | 1978-09-16 | 1980-04-11 | Rolls Royce | Aube a structure cristalline orientee pour moteur a turbine a gaz |
FR2515728A1 (fr) * | 1981-11-03 | 1983-05-06 | Rolls Royce | Soupape-champignon pour un moteur a combustion interne |
EP0100150A3 (en) * | 1982-07-28 | 1984-08-29 | Trw Inc. | Single crystal metal airfoil |
GB2301303A (en) * | 1980-12-30 | 1996-12-04 | Snecma | Manufacture of monocrystalline aerodynamic blades |
US7208116B2 (en) | 2000-09-29 | 2007-04-24 | Rolls-Royce Plc | Nickel base superalloy |
Families Citing this family (127)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3580324A (en) * | 1969-03-13 | 1971-05-25 | United Aircraft Corp | Double-oriented single crystal castings |
US3625275A (en) * | 1969-03-13 | 1971-12-07 | United Aircraft Corp | Apparatus and method for single-crystal casting |
US3677331A (en) * | 1969-07-14 | 1972-07-18 | Martin Marietta Corp | Casting process for nickel base alloys |
US3598172A (en) * | 1969-10-30 | 1971-08-10 | United Aircraft Corp | Process of casting with downward-unidirectional solidification |
US3650635A (en) * | 1970-03-09 | 1972-03-21 | Chromalloy American Corp | Turbine vanes |
US3787190A (en) * | 1970-06-01 | 1974-01-22 | United Aircraft Corp | Directionally solidified article |
US3690368A (en) * | 1970-08-14 | 1972-09-12 | United Aircraft Corp | Casting single crystal articles |
CH544217A (de) * | 1971-04-08 | 1973-11-15 | Bbc Sulzer Turbomaschinen | Gasturbinenschaufel |
US3767479A (en) * | 1972-02-14 | 1973-10-23 | Gen Electric | Multicomponent eutectics for high temperature applications |
US3973952A (en) * | 1973-06-11 | 1976-08-10 | The International Nickel Company, Inc. | Heat resistant alloy casting |
US3908733A (en) * | 1973-10-26 | 1975-09-30 | United Technologies Corp | Method and apparatus for control of alloy in columnar grain castings |
US3967355A (en) * | 1974-12-23 | 1976-07-06 | United Technologies Corporation | Composite single crystal article |
US4033792A (en) * | 1974-12-23 | 1977-07-05 | United Technologies Corporation | Composite single crystal article |
DE2508803C3 (de) * | 1975-02-28 | 1982-07-08 | Wacker-Chemitronic Gesellschaft für Elektronik-Grundstoffe mbH, 8263 Burghausen | Verfahren zur Herstellung plattenförmiger Siliciumkristalle mit Kolumnarstruktur |
US4093017A (en) * | 1975-12-29 | 1978-06-06 | Sherwood Refractories, Inc. | Cores for investment casting process |
US4116723A (en) * | 1976-11-17 | 1978-09-26 | United Technologies Corporation | Heat treated superalloy single crystal article and process |
US4209348A (en) * | 1976-11-17 | 1980-06-24 | United Technologies Corporation | Heat treated superalloy single crystal article and process |
US4133368A (en) * | 1977-08-01 | 1979-01-09 | United Technologies Corporation | Single crystal casting mold and method for making same |
US4240495A (en) * | 1978-04-17 | 1980-12-23 | General Motors Corporation | Method of making cast metal turbine wheel with integral radial columnar grain blades and equiaxed grain disc |
CA1142839A (en) * | 1978-12-13 | 1983-03-15 | Bruce E. Terkelsen | Method and apparatus for epitaxial solidification |
US4289570A (en) * | 1978-12-13 | 1981-09-15 | United Technologies Corporation | Seed and method for epitaxial solidification |
JPS55128801A (en) * | 1979-03-28 | 1980-10-06 | Fuji Elelctrochem Co Ltd | Manufacture of large single crystal of ferrite with uniform composition |
US4464094A (en) * | 1979-05-04 | 1984-08-07 | Trw Inc. | Turbine engine component and method of making the same |
US4764225A (en) * | 1979-05-29 | 1988-08-16 | Howmet Corporation | Alloys for high temperature applications |
US4345950A (en) * | 1980-04-21 | 1982-08-24 | General Electric Company | Method for making a composite grained cast article |
DE3114253A1 (de) * | 1980-05-09 | 1982-04-01 | United Technologies Corp., 06101 Hartford, Conn. | "superlegierung auf nickelbasis" |
US4372789A (en) * | 1980-08-07 | 1983-02-08 | General Electric Company | Directionally strengthened copper alloy parts for a gas turbine |
JPS57125613A (en) * | 1981-01-30 | 1982-08-05 | Yazaki Ind Chem Co Ltd | Warmth preserving container of pot planting part |
CA1209827A (en) * | 1981-08-05 | 1986-08-19 | David S. Duvall | Overlay coatings with high yttrium contents |
US4615865A (en) * | 1981-08-05 | 1986-10-07 | United Technologies Corporation | Overlay coatings with high yttrium contents |
US4409451A (en) * | 1981-08-31 | 1983-10-11 | United Technologies Corporation | Induction furnace having improved thermal profile |
US5399313A (en) * | 1981-10-02 | 1995-03-21 | General Electric Company | Nickel-based superalloys for producing single crystal articles having improved tolerance to low angle grain boundaries |
US5154884A (en) * | 1981-10-02 | 1992-10-13 | General Electric Company | Single crystal nickel-base superalloy article and method for making |
US4605452A (en) * | 1981-12-14 | 1986-08-12 | United Technologies Corporation | Single crystal articles having controlled secondary crystallographic orientation |
US4804311A (en) * | 1981-12-14 | 1989-02-14 | United Technologies Corporation | Transverse directional solidification of metal single crystal articles |
CA1339811C (en) * | 1981-12-30 | 1998-04-14 | David Noel Duhl | High strenght corrosion resistant nickel base single crystal article |
US4412577A (en) * | 1982-01-27 | 1983-11-01 | United Technologies Corporation | Control of seed melt-back during directional solidification of metals |
US4475582A (en) * | 1982-01-27 | 1984-10-09 | United Technologies Corporation | Casting a metal single crystal article using a seed crystal and a helix |
US4548255A (en) * | 1982-03-01 | 1985-10-22 | United Technologies Corporation | Mold with starter and selector sections for directional solidification casting |
EP0092496B1 (en) * | 1982-03-01 | 1986-10-01 | United Technologies Corporation | Mold with starter and selector sections for directional solidification casting |
US4475980A (en) * | 1982-06-01 | 1984-10-09 | United Technologies Corporation | Solid state production of multiple single crystal articles |
US4580613A (en) * | 1982-08-05 | 1986-04-08 | Howmet Turbine Components Corporation | Method and mold for casting articles having a predetermined crystalline orientation |
FR2734188B1 (fr) * | 1982-09-28 | 1997-07-18 | Snecma | Procede de fabrication de pieces monocristallines |
US4528048A (en) * | 1982-12-06 | 1985-07-09 | United Technologies Corporation | Mechanically worked single crystal article |
US6054096A (en) * | 1982-12-27 | 2000-04-25 | United Technologies Corporation | Stable heat treatable nickel superalloy single crystal articles and compositions |
US4610736A (en) * | 1983-03-23 | 1986-09-09 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Nickel base coating alloy |
US4612969A (en) * | 1983-04-27 | 1986-09-23 | Howmet Turbine Components Corporation | Method of and apparatus for casting articles with predetermined crystalline orientation |
US5413648A (en) * | 1983-12-27 | 1995-05-09 | United Technologies Corporation | Preparation of single crystal superalloys for post-casting heat treatment |
US4765850A (en) * | 1984-01-10 | 1988-08-23 | Allied-Signal Inc. | Single crystal nickel-base super alloy |
US4921549A (en) * | 1984-03-19 | 1990-05-01 | Inco Alloys International, Inc. | Promoting directional grain growth in objects |
US5551999A (en) * | 1984-04-23 | 1996-09-03 | United Technologies Corporation | Cyclic recovery heat treatment |
US4637448A (en) * | 1984-08-27 | 1987-01-20 | Westinghouse Electric Corp. | Method for production of combustion turbine blade having a single crystal portion |
US5100484A (en) * | 1985-10-15 | 1992-03-31 | General Electric Company | Heat treatment for nickel-base superalloys |
US6074602A (en) * | 1985-10-15 | 2000-06-13 | General Electric Company | Property-balanced nickel-base superalloys for producing single crystal articles |
JPS62103349A (ja) * | 1985-10-30 | 1987-05-13 | Agency Of Ind Science & Technol | 金属組織の制御方法 |
FR2593830B1 (fr) * | 1986-02-06 | 1988-04-08 | Snecma | Superalliage a matrice a base de nickel notamment elabore en metallurgie des poudres et disque de turbomachine constitue en cet alliage |
GB2234521B (en) * | 1986-03-27 | 1991-05-01 | Gen Electric | Nickel-base superalloys for producing single crystal articles having improved tolerance to low angle grain boundaries |
US4915907A (en) * | 1986-04-03 | 1990-04-10 | United Technologies Corporation | Single crystal articles having reduced anisotropy |
US4717432A (en) * | 1986-04-09 | 1988-01-05 | United Technologies Corporation | Varied heating rate solution heat treatment for superalloy castings |
US5077004A (en) * | 1986-05-07 | 1991-12-31 | Allied-Signal Inc. | Single crystal nickel-base superalloy for turbine components |
CA1315572C (en) * | 1986-05-13 | 1993-04-06 | Xuan Nguyen-Dinh | Phase stable single crystal materials |
US4849030A (en) * | 1986-06-09 | 1989-07-18 | General Electric Company | Dispersion strengthened single crystal alloys and method |
US4712604A (en) * | 1986-10-14 | 1987-12-15 | The United States Of America As Represented By The Secretary Of The Air Force | Apparatus for casting directionally solidified articles |
US4878965A (en) * | 1987-10-05 | 1989-11-07 | United Technologies Corporation | Oxidation resistant superalloy single crystals |
US4862947A (en) * | 1988-08-02 | 1989-09-05 | Pcc Airfoils, Inc. | Method of casting an article |
US5173255A (en) * | 1988-10-03 | 1992-12-22 | General Electric Company | Cast columnar grain hollow nickel base alloy articles and alloy and heat treatment for making |
US4921405A (en) * | 1988-11-10 | 1990-05-01 | Allied-Signal Inc. | Dual structure turbine blade |
US5062469A (en) * | 1989-07-19 | 1991-11-05 | Pcc Airfoils, Inc. | Mold and method for casting a single crystal metal article |
US4940073A (en) * | 1989-07-19 | 1990-07-10 | Pcc Airfoils, Inc. | Mold for casting a single crystal metal article |
US5061154A (en) * | 1989-12-11 | 1991-10-29 | Allied-Signal Inc. | Radial turbine rotor with improved saddle life |
US5074925A (en) * | 1990-06-25 | 1991-12-24 | The United States Of America As Represented By The Secretary Of The Air Force | Thermomechanical fabrication of net shape single crystal airfoils |
US5489194A (en) * | 1990-09-14 | 1996-02-06 | Hitachi, Ltd. | Gas turbine, gas turbine blade used therefor and manufacturing method for gas turbine blade |
DE4209227C1 (en) * | 1992-03-21 | 1993-05-06 | Access E.V., 5100 Aachen, De | Single crystal superalloy components, e.g. turbine blade or artificial hip joint |
US5273708A (en) * | 1992-06-23 | 1993-12-28 | Howmet Corporation | Method of making a dual alloy article |
US5451142A (en) * | 1994-03-29 | 1995-09-19 | United Technologies Corporation | Turbine engine blade having a zone of fine grains of a high strength composition at the blade root surface |
JP3010246B2 (ja) * | 1994-04-21 | 2000-02-21 | 大同メタル工業株式会社 | 高温用軸受合金 |
US5679180A (en) * | 1995-06-22 | 1997-10-21 | United Technologies Corporation | γ strengthened single crystal turbine blade alloy for hydrogen fueled propulsion systems |
CN1061704C (zh) * | 1995-11-14 | 2001-02-07 | 中国科学院金属研究所 | 一种镍铝基金属材料单晶的制备方法 |
JPH09225623A (ja) * | 1995-12-12 | 1997-09-02 | General Electric Co <Ge> | インベストメント鋳造超合金物品の環境抵抗の改善方法 |
DE69701900T2 (de) | 1996-02-09 | 2000-12-07 | Hitachi Metals, Ltd. | Hochfeste Superlegierung auf Nickelbasis für gerichtet erstarrte Giesteilen |
DE19614005A1 (de) * | 1996-04-09 | 1997-12-11 | Lyulka Saturn Inc | Gießform |
WO1999021680A2 (en) | 1997-10-27 | 1999-05-06 | Siemens Westinghouse Power Corporation | Turbine blades made from multiple single crystal cast superalloy segments |
US6325871B1 (en) | 1997-10-27 | 2001-12-04 | Siemens Westinghouse Power Corporation | Method of bonding cast superalloys |
US6217286B1 (en) * | 1998-06-26 | 2001-04-17 | General Electric Company | Unidirectionally solidified cast article and method of making |
US6096141A (en) * | 1998-08-03 | 2000-08-01 | General Electric Co. | Nickel-based superalloys exhibiting minimal grain defects |
JP2004538358A (ja) † | 1998-11-05 | 2004-12-24 | ロールス−ロイス・コーポレーション | 単結晶ベーンセグメント及びその製造方法 |
US6231692B1 (en) | 1999-01-28 | 2001-05-15 | Howmet Research Corporation | Nickel base superalloy with improved machinability and method of making thereof |
EP1076119A1 (en) * | 1999-08-11 | 2001-02-14 | ABB Alstom Power (Schweiz) AG | Apparatus and method for manufacture a directionally solidified columnar grained article |
US6551372B1 (en) | 1999-09-17 | 2003-04-22 | Rolls-Royce Corporation | High performance wrought powder metal articles and method of manufacture |
US6497272B1 (en) * | 1999-10-14 | 2002-12-24 | Howmet Research Corporation | Single crystal casting mold |
DE10038453A1 (de) * | 2000-08-07 | 2002-02-21 | Alstom Power Nv | Verfahren zur Herstellung eines gekühlten Feingussteils |
US6497968B2 (en) * | 2001-02-26 | 2002-12-24 | General Electric Company | Oxidation resistant coatings for molybdenum silicide-based composite articles |
GB2373467B (en) * | 2001-03-22 | 2004-04-14 | Rolls Royce Plc | Mould support arrangement |
US7575038B2 (en) * | 2001-06-11 | 2009-08-18 | Howmet Research Corporation | Single crystal seed |
DE50214427D1 (de) * | 2002-01-17 | 2010-06-24 | Siemens Ag | Gegossene Turbinenleitschaufel mit Hakensockel |
US20040115059A1 (en) * | 2002-12-12 | 2004-06-17 | Kehl Richard Eugene | Cored steam turbine bucket |
US7284958B2 (en) * | 2003-03-22 | 2007-10-23 | Allison Advanced Development Company | Separable blade platform |
EP1464791B1 (de) * | 2003-03-25 | 2008-12-10 | Siemens Aktiengesellschaft | Verfahren und Vorrichtung zur Herstellung einer Turbinenkomponente |
US6969240B2 (en) * | 2003-08-01 | 2005-11-29 | Honeywell International Inc. | Integral turbine composed of a cast single crystal blade ring diffusion bonded to a high strength disk |
US7011141B2 (en) * | 2003-09-02 | 2006-03-14 | General Electric Company | Apparatus and method for producing single crystal metallic objects |
GB2422641B (en) * | 2005-01-28 | 2007-11-14 | Rolls Royce Plc | Vane for a gas turbine engine |
US7824606B2 (en) * | 2006-09-21 | 2010-11-02 | Honeywell International Inc. | Nickel-based alloys and articles made therefrom |
US7905016B2 (en) * | 2007-04-10 | 2011-03-15 | Siemens Energy, Inc. | System for forming a gas cooled airfoil for use in a turbine engine |
JP5235383B2 (ja) * | 2007-11-07 | 2013-07-10 | 株式会社日立製作所 | Ni基単結晶合金及び鋳物 |
RU2402111C2 (ru) * | 2008-07-18 | 2010-10-20 | Общество С Ограниченной Ответственностью Научно-Производственное Объединение "Кристалл" | Кристаллическая пластина, прямоугольный брусок, компонент для производства термоэлектрических модулей и способ получения кристаллической пластины |
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DE490350C (de) * | 1927-09-27 | 1930-01-29 | Erftwerk Akt Ges | Verfahren zur Herstellung von Walz- und Pressbarren aus Nichteisenmetallen von grosser Kristallisationsgeschwindigkeit |
DE525514C (de) * | 1929-01-25 | 1931-05-26 | Ver Aluminium Werke Akt Ges | Verfahren zum Giessen von Barren und Bloecken aus Aluminium und seinen Legierungen unter Regelung der Erstarrung |
CH178282A (de) * | 1934-09-12 | 1935-07-15 | Bosshardt Ludwig Fritz Dr Phil | Verfahren zur Herstellung von Metallblöcken. |
US2712498A (en) * | 1948-06-01 | 1955-07-05 | Rolls Royce | Nickel chromium alloys having high creep strength at high temperatures |
DE1096040B (de) * | 1953-08-11 | 1960-12-29 | Wiggin & Co Ltd Henry | Verfahren zur Herstellung einer Nickellegierung hoher Kriechfestigkeit bei hohen Temperaturen |
US2951272A (en) * | 1958-09-22 | 1960-09-06 | Gen Electric | Method and apparatus for producing grain-oriented ingots |
US3008855A (en) * | 1959-01-26 | 1961-11-14 | Gen Motors Corp | Turbine blade and method of making same |
US3060065A (en) * | 1959-08-06 | 1962-10-23 | Theodore H Orem | Method for the growth of preferentially oriented single crystals of metals |
US3254994A (en) * | 1963-06-24 | 1966-06-07 | Trw Inc | Alloys having improved stress rupture properties |
US3248764A (en) * | 1964-01-08 | 1966-05-03 | Trw Inc | Method for improving grain structure and soundness in castings |
-
1966
- 1966-02-17 US US540114A patent/US3494709A/en not_active Expired - Lifetime
- 1966-05-09 GB GB20371/66A patent/GB1156721A/en not_active Expired
- 1966-05-18 DE DE19661533473 patent/DE1533473B1/de active Pending
- 1966-05-18 DE DE19661783103 patent/DE1783103B1/de active Pending
- 1966-05-23 CH CH741766A patent/CH489274A/de not_active IP Right Cessation
- 1966-05-27 SE SE07359/66A patent/SE330235B/xx unknown
- 1966-05-27 NL NL666607354A patent/NL147046B/xx not_active IP Right Cessation
- 1966-05-27 BE BE681776D patent/BE681776A/xx not_active IP Right Cessation
-
1968
- 1968-10-01 US US764171A patent/US3542120A/en not_active Expired - Lifetime
-
1969
- 1969-11-25 US US879772A patent/US3536121A/en not_active Expired - Lifetime
-
1971
- 1971-04-13 JP JP46023410A patent/JPS501455B1/ja active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2436254A1 (fr) * | 1978-09-16 | 1980-04-11 | Rolls Royce | Aube a structure cristalline orientee pour moteur a turbine a gaz |
GB2301303A (en) * | 1980-12-30 | 1996-12-04 | Snecma | Manufacture of monocrystalline aerodynamic blades |
GB2301303B (en) * | 1980-12-30 | 1997-10-22 | Snecma | Method for the manufacture of monocrystalline aerodynamic blades |
FR2515728A1 (fr) * | 1981-11-03 | 1983-05-06 | Rolls Royce | Soupape-champignon pour un moteur a combustion interne |
EP0100150A3 (en) * | 1982-07-28 | 1984-08-29 | Trw Inc. | Single crystal metal airfoil |
US7208116B2 (en) | 2000-09-29 | 2007-04-24 | Rolls-Royce Plc | Nickel base superalloy |
Also Published As
Publication number | Publication date |
---|---|
SE330235B (forum.php) | 1970-11-09 |
BE681776A (forum.php) | 1966-10-31 |
US3494709A (en) | 1970-02-10 |
DE1533473B1 (de) | 1970-11-12 |
CH489274A (de) | 1970-04-30 |
NL147046B (nl) | 1975-09-15 |
DE1783103B1 (de) | 1971-09-16 |
JPS501455B1 (forum.php) | 1975-01-18 |
US3542120A (en) | 1970-11-24 |
US3536121A (en) | 1970-10-27 |
NL6607354A (forum.php) | 1966-11-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PE | Patent expired |