FR1092136A - Improvements to the flow directing elements of turbo-machines - Google Patents
Improvements to the flow directing elements of turbo-machinesInfo
- Publication number
- FR1092136A FR1092136A FR1092136DA FR1092136A FR 1092136 A FR1092136 A FR 1092136A FR 1092136D A FR1092136D A FR 1092136DA FR 1092136 A FR1092136 A FR 1092136A
- Authority
- FR
- France
- Prior art keywords
- turbo
- machines
- flow directing
- directing elements
- elements
- 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
-
- 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
-
- 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
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- 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 |
---|---|---|---|
US323718XA | 1953-01-30 | 1953-01-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1092136A true FR1092136A (en) | 1955-04-19 |
Family
ID=21864607
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1092136D Expired FR1092136A (en) | 1953-01-30 | 1954-01-30 | Improvements to the flow directing elements of turbo-machines |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH323718A (en) |
FR (1) | FR1092136A (en) |
GB (1) | GB754217A (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB846277A (en) * | 1956-11-20 | 1960-08-31 | Rolls Royce | Turbine and compressor blades |
US3017159A (en) * | 1956-11-23 | 1962-01-16 | Curtiss Wright Corp | Hollow blade construction |
US2923525A (en) * | 1958-04-04 | 1960-02-02 | Orenda Engines Ltd | Hollow gas turbine blade |
GB893706A (en) * | 1960-01-05 | 1962-04-11 | Rolls Royce | Blades for fluid flow machines |
DE1173732B (en) * | 1960-06-08 | 1964-07-09 | Gen Motors Corp | Cast turbine blade |
GB2051964B (en) * | 1979-06-30 | 1983-01-12 | Rolls Royce | Turbine blade |
US5259730A (en) * | 1991-11-04 | 1993-11-09 | General Electric Company | Impingement cooled airfoil with bonding foil insert |
US6390774B1 (en) | 2000-02-02 | 2002-05-21 | General Electric Company | Gas turbine bucket cooling circuit and related process |
US6910864B2 (en) * | 2003-09-03 | 2005-06-28 | General Electric Company | Turbine bucket airfoil cooling hole location, style and configuration |
US8157527B2 (en) * | 2008-07-03 | 2012-04-17 | United Technologies Corporation | Airfoil with tapered radial cooling passage |
CN103216273A (en) * | 2013-04-17 | 2013-07-24 | 北京航空航天大学 | Efficient cooling turbine blade taking inner cooling channel surface as flow direction micro groove surface |
-
1954
- 1954-01-18 GB GB1375/54A patent/GB754217A/en not_active Expired
- 1954-01-30 CH CH323718D patent/CH323718A/en unknown
- 1954-01-30 FR FR1092136D patent/FR1092136A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
CH323718A (en) | 1957-08-15 |
GB754217A (en) | 1956-08-08 |
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