GB1307338A - Turbine blades - Google Patents
Turbine bladesInfo
- Publication number
- GB1307338A GB1307338A GB2002171A GB2002171A GB1307338A GB 1307338 A GB1307338 A GB 1307338A GB 2002171 A GB2002171 A GB 2002171A GB 2002171 A GB2002171 A GB 2002171A GB 1307338 A GB1307338 A GB 1307338A
- Authority
- GB
- United Kingdom
- Prior art keywords
- brazing
- welding
- core
- sheath
- 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
- 238000005219 brazing Methods 0.000 abstract 3
- 238000003466 welding Methods 0.000 abstract 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 abstract 1
- 239000004411 aluminium Substances 0.000 abstract 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract 1
- 229910052782 aluminium Inorganic materials 0.000 abstract 1
- 229910052802 copper Inorganic materials 0.000 abstract 1
- 239000010949 copper Substances 0.000 abstract 1
- 238000009792 diffusion process Methods 0.000 abstract 1
- 239000007789 gas Substances 0.000 abstract 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 abstract 1
- 229910052737 gold Inorganic materials 0.000 abstract 1
- 239000010931 gold Substances 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 abstract 1
- 239000001257 hydrogen Substances 0.000 abstract 1
- 229910052739 hydrogen Inorganic materials 0.000 abstract 1
- 238000007747 plating Methods 0.000 abstract 1
- 238000005476 soldering Methods 0.000 abstract 1
- 239000007787 solid Substances 0.000 abstract 1
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
- F01D5/185—Liquid cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/80—Platforms for stationary or moving blades
- F05B2240/801—Platforms for stationary or moving blades cooled platforms
-
- 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
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
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 |
|---|---|---|---|
| US780570A | 1970-02-02 | 1970-02-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1307338A true GB1307338A (en) | 1973-02-21 |
Family
ID=21728216
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2002171A Expired GB1307338A (en) | 1970-02-02 | 1971-04-19 | Turbine blades |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US3619076A (enExample) |
| JP (1) | JPS545048B1 (enExample) |
| DE (1) | DE2104482C3 (enExample) |
| FR (1) | FR2080425A5 (enExample) |
| GB (1) | GB1307338A (enExample) |
| NL (1) | NL169627C (enExample) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4623087A (en) * | 1983-05-26 | 1986-11-18 | Rolls-Royce Limited | Application of coatings to articles |
| US8858182B2 (en) | 2011-06-28 | 2014-10-14 | United Technologies Corporation | Fan blade with sheath |
Families Citing this family (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1801475B2 (de) * | 1968-10-05 | 1971-08-12 | Daimler Benz Ag, 7000 Stuttgart | Luftgekuehlte turbinenschaufel |
| US3936227A (en) * | 1973-08-02 | 1976-02-03 | General Electric Company | Combined coolant feed and dovetailed bucket retainer ring |
| US3980411A (en) * | 1975-10-20 | 1976-09-14 | United Technologies Corporation | Aerodynamic seal for a rotary machine |
| US4111604A (en) * | 1976-07-12 | 1978-09-05 | General Electric Company | Bucket tip construction for open circuit liquid cooled turbines |
| US4134709A (en) * | 1976-08-23 | 1979-01-16 | General Electric Company | Thermosyphon liquid cooled turbine bucket |
| US4119390A (en) * | 1976-11-19 | 1978-10-10 | General Electric Company | Liquid-cooled, turbine bucket with enhanced heat transfer performance |
| US4156582A (en) * | 1976-12-13 | 1979-05-29 | General Electric Company | Liquid cooled gas turbine buckets |
| US4090810A (en) * | 1977-03-23 | 1978-05-23 | General Electric Company | Liquid-cooled turbine bucket with enhanced heat transfer performance |
| US4137619A (en) * | 1977-10-03 | 1979-02-06 | General Electric Company | Method of fabricating composite structures for water cooled gas turbine components |
| US4158526A (en) * | 1978-01-09 | 1979-06-19 | General Electric Company | Turbine assembly including a rotatable liquid collection ring |
| US4185369A (en) * | 1978-03-22 | 1980-01-29 | General Electric Company | Method of manufacture of cooled turbine or compressor buckets |
| DE3211139C1 (de) * | 1982-03-26 | 1983-08-11 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Axialturbinenschaufel,insbesondere Axialturbinenlaufschaufel fuer Gasturbinentriebwerke |
| US4684323A (en) * | 1985-12-23 | 1987-08-04 | United Technologies Corporation | Film cooling passages with curved corners |
| US4726735A (en) * | 1985-12-23 | 1988-02-23 | United Technologies Corporation | Film cooling slot with metered flow |
| US4676719A (en) * | 1985-12-23 | 1987-06-30 | United Technologies Corporation | Film coolant passages for cast hollow airfoils |
| US4653983A (en) * | 1985-12-23 | 1987-03-31 | United Technologies Corporation | Cross-flow film cooling passages |
| US4705455A (en) * | 1985-12-23 | 1987-11-10 | United Technologies Corporation | Convergent-divergent film coolant passage |
| US4664597A (en) * | 1985-12-23 | 1987-05-12 | United Technologies Corporation | Coolant passages with full coverage film cooling slot |
| US4669957A (en) * | 1985-12-23 | 1987-06-02 | United Technologies Corporation | Film coolant passage with swirl diffuser |
| US4738588A (en) * | 1985-12-23 | 1988-04-19 | Field Robert E | Film cooling passages with step diffuser |
| US4666368A (en) * | 1986-05-01 | 1987-05-19 | General Electric Company | Swirl nozzle for a cooling system in gas turbine engines |
| WO1999060253A1 (de) * | 1998-05-18 | 1999-11-25 | Siemens Aktiengesellschaft | Gekühlte turbinenschaufelplattform |
| US6565312B1 (en) * | 2001-12-19 | 2003-05-20 | The Boeing Company | Fluid-cooled turbine blades |
| US6699015B2 (en) | 2002-02-19 | 2004-03-02 | The Boeing Company | Blades having coolant channels lined with a shape memory alloy and an associated fabrication method |
| US7488156B2 (en) * | 2006-06-06 | 2009-02-10 | Siemens Energy, Inc. | Turbine airfoil with floating wall mechanism and multi-metering diffusion technique |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3075744A (en) * | 1960-08-16 | 1963-01-29 | United Aircraft Corp | Turbine nozzle vane mounting means |
| US3446480A (en) * | 1966-12-19 | 1969-05-27 | Gen Motors Corp | Turbine rotor |
| US3446481A (en) * | 1967-03-24 | 1969-05-27 | Gen Electric | Liquid cooled turbine rotor |
-
1970
- 1970-02-02 US US7805A patent/US3619076A/en not_active Expired - Lifetime
-
1971
- 1971-01-20 FR FR7101760A patent/FR2080425A5/fr not_active Expired
- 1971-01-26 NL NLAANVRAGE7100990,A patent/NL169627C/xx not_active IP Right Cessation
- 1971-02-01 DE DE2104482A patent/DE2104482C3/de not_active Expired
- 1971-02-02 JP JP364671A patent/JPS545048B1/ja active Pending
- 1971-04-19 GB GB2002171A patent/GB1307338A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4623087A (en) * | 1983-05-26 | 1986-11-18 | Rolls-Royce Limited | Application of coatings to articles |
| US8858182B2 (en) | 2011-06-28 | 2014-10-14 | United Technologies Corporation | Fan blade with sheath |
Also Published As
| Publication number | Publication date |
|---|---|
| US3619076A (en) | 1971-11-09 |
| NL7100990A (enExample) | 1971-08-04 |
| NL169627B (nl) | 1982-03-01 |
| DE2104482C3 (de) | 1980-05-14 |
| DE2104482A1 (de) | 1971-08-12 |
| DE2104482B2 (de) | 1979-09-06 |
| JPS545048B1 (enExample) | 1979-03-13 |
| NL169627C (nl) | 1982-08-02 |
| FR2080425A5 (enExample) | 1971-11-12 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed [section 19, patents act 1949] | ||
| PCNP | Patent ceased through non-payment of renewal fee |