FR1177035A - Procédé et dispositif de refroidissement d'organes de machines - Google Patents
Procédé et dispositif de refroidissement d'organes de machinesInfo
- Publication number
- FR1177035A FR1177035A FR1177035DA FR1177035A FR 1177035 A FR1177035 A FR 1177035A FR 1177035D A FR1177035D A FR 1177035DA FR 1177035 A FR1177035 A FR 1177035A
- Authority
- FR
- France
- Prior art keywords
- machine parts
- cooling machine
- cooling
- parts
- machine
- 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
-
- 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
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
- F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
-
- 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
- F01D5/182—Transpiration cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1092255X | 1957-05-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1177035A true FR1177035A (fr) | 1959-04-20 |
Family
ID=9615865
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1177035D Expired FR1177035A (fr) | 1957-05-28 | 1957-05-28 | Procédé et dispositif de refroidissement d'organes de machines |
Country Status (4)
Country | Link |
---|---|
US (1) | US3032314A (fr) |
DE (1) | DE1092255B (fr) |
FR (1) | FR1177035A (fr) |
GB (1) | GB853328A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1204021B (de) * | 1959-04-27 | 1965-10-28 | Rolls Royce | Schaufel fuer Axialstroemungsmaschinen, insbesondere Gasturbinen |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3191908A (en) * | 1961-05-02 | 1965-06-29 | Rolls Royce | Blades for fluid flow machines |
US3171631A (en) * | 1962-12-05 | 1965-03-02 | Gen Motors Corp | Turbine blade |
US3319593A (en) * | 1962-12-24 | 1967-05-16 | Papst Hermann | Boundary layer control |
US3316714A (en) * | 1963-06-20 | 1967-05-02 | Rolls Royce | Gas turbine engine combustion equipment |
US3346235A (en) * | 1963-12-23 | 1967-10-10 | Papst Hermann | Boundary layer control |
GB1034260A (en) * | 1964-12-02 | 1966-06-29 | Rolls Royce | Aerofoil-shaped blade for use in a fluid flow machine |
US3240468A (en) * | 1964-12-28 | 1966-03-15 | Curtiss Wright Corp | Transpiration cooled blades for turbines, compressors, and the like |
US3301527A (en) * | 1965-05-03 | 1967-01-31 | Gen Electric | Turbine diaphragm structure |
FR1503348A (fr) * | 1965-12-11 | 1967-11-24 | Daimler Benz Ag | Aube pour turbines à gaz, en particulier pour réacteurs d'avions |
GB1070480A (en) * | 1966-02-01 | 1967-06-01 | Rolls Royce | Aerofoil shaped blade for a fluid flow machine such as a gas turbine engine |
US3540810A (en) * | 1966-03-17 | 1970-11-17 | Gen Electric | Slanted partition for hollow airfoil vane insert |
US3574481A (en) * | 1968-05-09 | 1971-04-13 | James A Pyne Jr | Variable area cooled airfoil construction for gas turbines |
US3700348A (en) * | 1968-08-13 | 1972-10-24 | Gen Electric | Turbomachinery blade structure |
US3715170A (en) * | 1970-12-11 | 1973-02-06 | Gen Electric | Cooled turbine blade |
US3767322A (en) * | 1971-07-30 | 1973-10-23 | Westinghouse Electric Corp | Internal cooling for turbine vanes |
US3806275A (en) * | 1972-08-30 | 1974-04-23 | Gen Motors Corp | Cooled airfoil |
US3806276A (en) * | 1972-08-30 | 1974-04-23 | Gen Motors Corp | Cooled turbine blade |
CH584347A5 (fr) * | 1974-11-08 | 1977-01-31 | Bbc Sulzer Turbomaschinen | |
GB1564608A (en) * | 1975-12-20 | 1980-04-10 | Rolls Royce | Means for cooling a surface by the impingement of a cooling fluid |
DE3003347A1 (de) * | 1979-12-20 | 1981-06-25 | BBC AG Brown, Boveri & Cie., Baden, Aargau | Gekuehlte wand |
IN163070B (fr) * | 1984-11-15 | 1988-08-06 | Westinghouse Electric Corp | |
US6237344B1 (en) | 1998-07-20 | 2001-05-29 | General Electric Company | Dimpled impingement baffle |
US6183192B1 (en) * | 1999-03-22 | 2001-02-06 | General Electric Company | Durable turbine nozzle |
GB2439330B (en) | 2006-06-22 | 2008-09-17 | Rolls Royce Plc | Aerofoil |
US9719362B2 (en) * | 2013-04-24 | 2017-08-01 | Honeywell International Inc. | Turbine nozzles and methods of manufacturing the same |
EP2949871B1 (fr) * | 2014-05-07 | 2017-03-01 | United Technologies Corporation | Segment d'aube variable |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE432599A (fr) * | 1938-02-08 | |||
CH237475A (de) * | 1942-06-09 | 1945-04-30 | Vorkauf Heinrich | Verfahren und Vorrichtung zur Kühlung von Gasturbinenschaufeln. |
DE906636C (de) * | 1944-01-23 | 1954-03-15 | Herwig Kress Dr Ing | Gas- oder Abgasturbinen mit Hohlschaufelkuehlung |
US2514105A (en) * | 1945-12-07 | 1950-07-04 | Thomas Wilfred | Airfoil conditioning means |
BE498667A (fr) * | 1949-08-27 | |||
US2746671A (en) * | 1950-04-14 | 1956-05-22 | United Aircraft Corp | Compressor deicing and thrust balancing arrangement |
DE949954C (de) * | 1952-02-09 | 1956-09-27 | Helmut Reining | Vorrichtung an Kuehlrahmen fuer Siemens-Martin-OEfen oder andere Industrieoefen |
US2787049A (en) * | 1952-05-23 | 1957-04-02 | Stalkcr Dev Company | Process of fabricating blades for turbines, compressors and the like |
US2873944A (en) * | 1952-09-10 | 1959-02-17 | Gen Motors Corp | Turbine blade cooling |
GB740597A (en) * | 1953-11-07 | 1955-11-16 | Gen Motors Corp | Improvements relating to gas turbine or compressor blades |
US2780435A (en) * | 1953-01-12 | 1957-02-05 | Jackson Thomas Woodrow | Turbine blade cooling structure |
GB753224A (en) * | 1953-04-13 | 1956-07-18 | Rolls Royce | Improvements in or relating to blading for turbines or compressors |
US2859011A (en) * | 1953-07-27 | 1958-11-04 | Gen Motors Corp | Turbine bucket and liner |
US2851216A (en) * | 1954-01-13 | 1958-09-09 | Schwarzkopf Dev Co | Device adapted for respiration cooling and process of making same |
-
1957
- 1957-05-28 FR FR1177035D patent/FR1177035A/fr not_active Expired
-
1958
- 1958-05-14 US US735243A patent/US3032314A/en not_active Expired - Lifetime
- 1958-05-15 GB GB15684/58A patent/GB853328A/en not_active Expired
- 1958-05-19 DE DES58280A patent/DE1092255B/de active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1204021B (de) * | 1959-04-27 | 1965-10-28 | Rolls Royce | Schaufel fuer Axialstroemungsmaschinen, insbesondere Gasturbinen |
Also Published As
Publication number | Publication date |
---|---|
DE1092255B (de) | 1960-11-03 |
GB853328A (en) | 1960-11-02 |
US3032314A (en) | 1962-05-01 |
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