FR1246503A - Ailette moulée de turbine et son procédé de fabrication - Google Patents
Ailette moulée de turbine et son procédé de fabricationInfo
- Publication number
- FR1246503A FR1246503A FR816405A FR816405A FR1246503A FR 1246503 A FR1246503 A FR 1246503A FR 816405 A FR816405 A FR 816405A FR 816405 A FR816405 A FR 816405A FR 1246503 A FR1246503 A FR 1246503A
- Authority
- FR
- France
- Prior art keywords
- manufacturing process
- turbine blade
- molded turbine
- molded
- blade
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
- B22C9/106—Vented or reinforced cores
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US78842959A | 1959-01-22 | 1959-01-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1246503A true FR1246503A (fr) | 1960-11-18 |
Family
ID=25144463
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR816405A Expired FR1246503A (fr) | 1959-01-22 | 1960-01-22 | Ailette moulée de turbine et son procédé de fabrication |
Country Status (4)
Country | Link |
---|---|
CH (1) | CH373524A (fr) |
DE (1) | DE1195910B (fr) |
FR (1) | FR1246503A (fr) |
GB (1) | GB872705A (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2502529A1 (fr) * | 1981-03-25 | 1982-10-01 | Rolls Royce | Procede de fabrication de la partie aerodynamiquement profilee d'une aube de moteur a turbine a gaz |
FR2504828A1 (fr) * | 1977-07-22 | 1982-11-05 | Rolls Royce | Procede de fabrication, par moulage, d'un corps creux de formes complexes |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB895077A (en) * | 1959-12-09 | 1962-05-02 | Rolls Royce | Blades for fluid flow machines such as axial flow turbines |
US3834831A (en) * | 1973-01-23 | 1974-09-10 | Westinghouse Electric Corp | Blade shank cooling arrangement |
US4407632A (en) * | 1981-06-26 | 1983-10-04 | United Technologies Corporation | Airfoil pedestaled trailing edge region cooling configuration |
US4595340A (en) * | 1984-07-30 | 1986-06-17 | General Electric Company | Gas turbine bladed disk assembly |
GB2237846B (en) * | 1989-11-09 | 1993-12-15 | Rolls Royce Plc | Rim parasitic weight reduction |
US5690472A (en) * | 1992-02-03 | 1997-11-25 | General Electric Company | Internal cooling of turbine airfoil wall using mesh cooling hole arrangement |
GB2270718A (en) * | 1992-09-22 | 1994-03-23 | Rolls Royce Plc | Single crystal turbine blades having pedestals. |
FR2698126B1 (fr) * | 1992-11-18 | 1994-12-16 | Snecma | Aube creuse de soufflante ou compresseur de turbomachine. |
EP0935052B1 (fr) * | 1998-02-04 | 2006-05-03 | Mitsubishi Heavy Industries, Ltd. | Aube rotorique pour turbine à gaz |
US7217094B2 (en) | 2004-10-18 | 2007-05-15 | United Technologies Corporation | Airfoil with large fillet and micro-circuit cooling |
US20070240845A1 (en) * | 2006-04-18 | 2007-10-18 | Graham Stephen D | Investment cast article and method of production thereof |
EP2168698A1 (fr) * | 2008-09-26 | 2010-03-31 | Siemens Aktiengesellschaft | Pièce de formage dotée d'un module séparé pour âmes, procédé de fabrication d'un moule en fonte, moule en fonte céramique et pièce en fonte |
GB201514793D0 (en) | 2015-08-20 | 2015-10-07 | Rolls Royce Plc | Cooling of turbine blades and method for turbine blade manufacture |
US10940531B1 (en) * | 2019-10-31 | 2021-03-09 | The Boeing Company | Methods and systems for improving a surface finish of an investment casting |
CN114988852B (zh) * | 2022-05-13 | 2023-09-05 | 潍坊科技学院 | 一种具有多层夹层结构陶瓷型芯的制备方法 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE737479C (de) * | 1939-01-26 | 1943-07-15 | Versuchsanstalt Fuer Luftfahrt | Gasturbinenschaufel |
DE860438C (de) * | 1941-03-28 | 1952-12-22 | Versuchsanstalt Fuer Luftfahrt | Hohlschaufel fuer Gas- oder Abgasturbinen |
DE904610C (de) * | 1944-04-22 | 1954-02-22 | Siemens Ag | Luftgekuehlte Hohlschaufel fuer Gasturbinen, bei der die Kuehlluft vom Schaufelfuss her in die Schaufel eintritt |
GB731292A (en) * | 1951-10-10 | 1955-06-08 | Gen Motors Corp | Improvements in processes of making turbine and compressor blades |
US2801073A (en) * | 1952-06-30 | 1957-07-30 | United Aircraft Corp | Hollow sheet metal blade or vane construction |
GB742476A (en) * | 1952-10-31 | 1955-12-30 | Rolls Royce | Improvements in or relating to bladed stator and rotor constructions for fluid machines such as axial-flow turbines or compressors |
DE1032898B (de) * | 1953-09-19 | 1958-06-26 | Miguel Schmitt | Giesskern und Verfahren zur Herstellung von Gussteilen |
GB781492A (en) * | 1954-12-10 | 1957-08-21 | Chrysler Corp | Improvements in or relating to an air cooled turbine blade |
-
1960
- 1960-01-12 GB GB107260A patent/GB872705A/en not_active Expired
- 1960-01-13 DE DEG28786A patent/DE1195910B/de active Pending
- 1960-01-21 CH CH66160A patent/CH373524A/de unknown
- 1960-01-22 FR FR816405A patent/FR1246503A/fr not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2504828A1 (fr) * | 1977-07-22 | 1982-11-05 | Rolls Royce | Procede de fabrication, par moulage, d'un corps creux de formes complexes |
FR2502529A1 (fr) * | 1981-03-25 | 1982-10-01 | Rolls Royce | Procede de fabrication de la partie aerodynamiquement profilee d'une aube de moteur a turbine a gaz |
Also Published As
Publication number | Publication date |
---|---|
CH373524A (de) | 1963-11-30 |
DE1195910B (de) | 1965-07-01 |
GB872705A (en) | 1961-07-12 |
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