FR1022398A - Improvements to turbine blades and the like - Google Patents
Improvements to turbine blades and the likeInfo
- Publication number
- FR1022398A FR1022398A FR1022398DA FR1022398A FR 1022398 A FR1022398 A FR 1022398A FR 1022398D A FR1022398D A FR 1022398DA FR 1022398 A FR1022398 A FR 1022398A
- Authority
- FR
- France
- Prior art keywords
- turbine blades
- turbine
- blades
- 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
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/25—Three-dimensional helical
-
- 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
- F05D2260/2212—Improvement of heat transfer by creating turbulence
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 |
|---|---|---|---|
| GB286626X | 1949-07-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR1022398A true FR1022398A (en) | 1953-03-04 |
Family
ID=10279147
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1022398D Expired FR1022398A (en) | 1949-07-06 | 1950-07-05 | Improvements to turbine blades and the like |
| FR66874D Expired FR66874E (en) | 1949-07-06 | 1953-06-02 | Improvements to turbine blades or the like |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR66874D Expired FR66874E (en) | 1949-07-06 | 1953-06-02 | Improvements to turbine blades or the like |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US2843354A (en) |
| BE (1) | BE496812A (en) |
| CH (1) | CH286626A (en) |
| FR (2) | FR1022398A (en) |
| GB (2) | GB680118A (en) |
| NL (1) | NL73916C (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1031056B (en) * | 1954-10-18 | 1958-05-29 | Parsons & Marine Eng Turbine | Cooling arrangement for cooling parts exposed to a hot gas flow |
| US2921769A (en) * | 1953-06-08 | 1960-01-19 | Peerless Turbine Corp | Turbine rotor |
| DE1157432B (en) * | 1959-12-09 | 1963-11-14 | Rolls Royce | Blade for flow machines, especially for axial gas turbines |
| DE1265495B (en) * | 1963-08-30 | 1968-04-04 | Gen Electric | Hollow stator or rotor blade |
| FR2371574A1 (en) * | 1976-11-19 | 1978-06-16 | Gen Electric | Water cooled blade for gas turbine - has flow equalising threads in each radial water passage |
| FR2393142A1 (en) * | 1976-11-19 | 1978-12-29 | Gen Electric | MOBILE TURBINE VANE COOLED BY LIQUID |
| DE2825801A1 (en) * | 1977-06-15 | 1979-01-04 | Gen Electric | LIQUID-COOLED TURBINE SHOVEL WITH IMPROVED HEAT TRANSFER CAPACITY |
| CN112483191A (en) * | 2020-11-30 | 2021-03-12 | 日照黎阳工业装备有限公司 | Turbine blade suitable for gas turbine possesses heat convection function |
Families Citing this family (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2999669A (en) * | 1958-11-21 | 1961-09-12 | Westinghouse Electric Corp | Damping apparatus |
| US3370829A (en) * | 1965-12-20 | 1968-02-27 | Avco Corp | Gas turbine blade construction |
| FR2098558A5 (en) * | 1970-07-20 | 1972-03-10 | Onera (Off Nat Aerospatiale) | |
| US4080095A (en) * | 1976-09-02 | 1978-03-21 | Westinghouse Electric Corporation | Cooled turbine vane |
| US4383854A (en) * | 1980-12-29 | 1983-05-17 | General Electric Company | Method of creating a controlled interior surface configuration of passages within a substrate |
| GB2163219B (en) * | 1981-10-31 | 1986-08-13 | Rolls Royce | Cooled turbine blade |
| DE3416087A1 (en) * | 1984-04-30 | 1985-10-31 | Klöckner-Humboldt-Deutz AG, 5000 Köln | COOLED TURBINE BLADE |
| US5002460A (en) * | 1989-10-02 | 1991-03-26 | General Electric Company | Internally cooled airfoil blade |
| US5704763A (en) * | 1990-08-01 | 1998-01-06 | General Electric Company | Shear jet cooling passages for internally cooled machine elements |
| US5253976A (en) * | 1991-11-19 | 1993-10-19 | General Electric Company | Integrated steam and air cooling for combined cycle gas turbines |
| US5320483A (en) * | 1992-12-30 | 1994-06-14 | General Electric Company | Steam and air cooling for stator stage of a turbine |
| US5486093A (en) * | 1993-09-08 | 1996-01-23 | United Technologies Corporation | Leading edge cooling of turbine airfoils |
| FR2765265B1 (en) * | 1997-06-26 | 1999-08-20 | Snecma | BLADED COOLING BY HELICAL RAMP, CASCADE IMPACT AND BY BRIDGE SYSTEM IN A DOUBLE SKIN |
| EP1621730B1 (en) * | 2004-07-26 | 2008-10-08 | Siemens Aktiengesellschaft | Cooled turbomachinery element and casting method thereof |
| US7163373B2 (en) * | 2005-02-02 | 2007-01-16 | Siemens Power Generation, Inc. | Vortex dissipation device for a cooling system within a turbine blade of a turbine engine |
| US8297927B1 (en) * | 2008-03-04 | 2012-10-30 | Florida Turbine Technologies, Inc. | Near wall multiple impingement serpentine flow cooled airfoil |
| EP2372087A1 (en) * | 2010-03-26 | 2011-10-05 | Siemens Aktiengesellschaft | Components with an external wall which can be exposed to a hot gas of a gas turbine and method for producing such a component |
| DE102012017491A1 (en) | 2012-09-04 | 2014-03-06 | Rolls-Royce Deutschland Ltd & Co Kg | Turbine blade of a gas turbine with swirl-generating element |
| GB2518379A (en) * | 2013-09-19 | 2015-03-25 | Rolls Royce Deutschland | Aerofoil cooling system and method |
| US8864438B1 (en) * | 2013-12-05 | 2014-10-21 | Siemens Energy, Inc. | Flow control insert in cooling passage for turbine vane |
| US9932835B2 (en) * | 2014-05-23 | 2018-04-03 | United Technologies Corporation | Airfoil cooling device and method of manufacture |
| WO2016014056A1 (en) * | 2014-07-24 | 2016-01-28 | Siemens Aktiengesellschaft | Turbine airfoil cooling system with spanwise extending flow blockers |
| EP3350414A1 (en) * | 2015-11-10 | 2018-07-25 | Siemens Aktiengesellschaft | Laminated airfoil for a gas turbine |
| PL232314B1 (en) * | 2016-05-06 | 2019-06-28 | Gen Electric | Fluid-flow machine equipped with the clearance adjustment system |
| US10309246B2 (en) | 2016-06-07 | 2019-06-04 | General Electric Company | Passive clearance control system for gas turbomachine |
| US10605093B2 (en) | 2016-07-12 | 2020-03-31 | General Electric Company | Heat transfer device and related turbine airfoil |
| US10392944B2 (en) | 2016-07-12 | 2019-08-27 | General Electric Company | Turbomachine component having impingement heat transfer feature, related turbomachine and storage medium |
| US10738622B2 (en) | 2016-08-09 | 2020-08-11 | General Electric Company | Components having outer wall recesses for impingement cooling |
| US11149550B2 (en) * | 2019-02-07 | 2021-10-19 | Raytheon Technologies Corporation | Blade neck transition |
| US10871074B2 (en) | 2019-02-28 | 2020-12-22 | Raytheon Technologies Corporation | Blade/vane cooling passages |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US970349A (en) * | 1910-02-25 | 1910-09-13 | Theodore B Stubbs | Crude-oil burner. |
| US1864742A (en) * | 1923-06-15 | 1932-06-28 | Charles N Koch | Combustion turbine and method of burning fuel |
| US1928504A (en) * | 1932-01-09 | 1933-09-26 | Holzwarth Gas Turbine Co | Cooled nozzle segment for combustion gas turbines |
| US2043644A (en) * | 1933-09-21 | 1936-06-09 | Cyril C Young | Heat transfer apparatus |
| GB426885A (en) * | 1933-11-03 | 1935-04-11 | Dewandre Co Ltd C | Improvements in or relating to heat transmitting tubes |
| CH213483A (en) * | 1938-11-23 | 1941-02-15 | Porsche Kg | Impeller for internal combustion or steam turbines and process for producing the same. |
| US2297446A (en) * | 1938-12-03 | 1942-09-29 | Zellbeck Gustav | Hollow blade for exhaust gas turbine rotors |
| US2407531A (en) * | 1942-05-02 | 1946-09-10 | Fed Reserve Bank | Elastic fluid mechanism |
| US2520373A (en) * | 1945-01-24 | 1950-08-29 | Lockheed Aircraft Corp | Turbine blade and method of making the same |
| GB625693A (en) * | 1946-10-25 | 1949-07-01 | Brush Electrical Eng | Improvements in and relating to turbine blades |
| US2581252A (en) * | 1947-12-31 | 1952-01-01 | Sintercast Corp America | Powder metallurgy articles |
| US2665881A (en) * | 1948-06-15 | 1954-01-12 | Chrysler Corp | Cooled turbine blade |
| US2568726A (en) * | 1949-08-03 | 1951-09-25 | Franz Anselm | Air-cooled turbine blade |
-
0
- BE BE496812D patent/BE496812A/xx unknown
- NL NL73916D patent/NL73916C/xx active
-
1949
- 1949-07-06 GB GB17900/49A patent/GB680118A/en not_active Expired
-
1950
- 1950-06-30 US US171263A patent/US2843354A/en not_active Expired - Lifetime
- 1950-07-05 CH CH286626D patent/CH286626A/en unknown
- 1950-07-05 FR FR1022398D patent/FR1022398A/en not_active Expired
-
1952
- 1952-06-03 GB GB14028/52A patent/GB728834A/en not_active Expired
-
1953
- 1953-06-02 FR FR66874D patent/FR66874E/en not_active Expired
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2921769A (en) * | 1953-06-08 | 1960-01-19 | Peerless Turbine Corp | Turbine rotor |
| DE1031056B (en) * | 1954-10-18 | 1958-05-29 | Parsons & Marine Eng Turbine | Cooling arrangement for cooling parts exposed to a hot gas flow |
| DE1157432B (en) * | 1959-12-09 | 1963-11-14 | Rolls Royce | Blade for flow machines, especially for axial gas turbines |
| DE1265495B (en) * | 1963-08-30 | 1968-04-04 | Gen Electric | Hollow stator or rotor blade |
| FR2371574A1 (en) * | 1976-11-19 | 1978-06-16 | Gen Electric | Water cooled blade for gas turbine - has flow equalising threads in each radial water passage |
| FR2393142A1 (en) * | 1976-11-19 | 1978-12-29 | Gen Electric | MOBILE TURBINE VANE COOLED BY LIQUID |
| DE2825801A1 (en) * | 1977-06-15 | 1979-01-04 | Gen Electric | LIQUID-COOLED TURBINE SHOVEL WITH IMPROVED HEAT TRANSFER CAPACITY |
| CN112483191A (en) * | 2020-11-30 | 2021-03-12 | 日照黎阳工业装备有限公司 | Turbine blade suitable for gas turbine possesses heat convection function |
Also Published As
| Publication number | Publication date |
|---|---|
| FR66874E (en) | 1957-10-31 |
| US2843354A (en) | 1958-07-15 |
| CH286626A (en) | 1952-10-31 |
| GB680118A (en) | 1952-10-01 |
| BE496812A (en) | 1900-01-01 |
| GB728834A (en) | 1955-04-27 |
| NL73916C (en) | 1900-01-01 |
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