CA1042349A - Stator vane assembly for gas turbines - Google Patents
Stator vane assembly for gas turbinesInfo
- Publication number
- CA1042349A CA1042349A CA269,632A CA269632A CA1042349A CA 1042349 A CA1042349 A CA 1042349A CA 269632 A CA269632 A CA 269632A CA 1042349 A CA1042349 A CA 1042349A
- Authority
- CA
- Canada
- Prior art keywords
- vane
- tenon
- airfoil
- end cap
- tenons
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/284—Selection of ceramic materials
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- 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
- F05D2240/10—Stators
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/659,869 US4053257A (en) | 1976-02-20 | 1976-02-20 | Stator vane assembly for gas turbines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1042349A true CA1042349A (en) | 1978-11-14 |
Family
ID=24647165
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA269,632A Expired CA1042349A (en) | 1976-02-20 | 1977-01-13 | Stator vane assembly for gas turbines |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US4053257A (Direct) |
| JP (1) | JPS52115909A (Direct) |
| CA (1) | CA1042349A (Direct) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH676735A5 (Direct) * | 1988-08-03 | 1991-02-28 | Asea Brown Boveri | |
| US5411368A (en) * | 1993-11-08 | 1995-05-02 | Allied-Signal Inc. | Ceramic-to-metal stator vane assembly with braze |
| US10132186B2 (en) * | 2015-08-13 | 2018-11-20 | General Electric Company | System and method for supporting a turbine shroud |
| US11448078B2 (en) * | 2020-04-23 | 2022-09-20 | Raytheon Technologies Corporation | Spring loaded airfoil vane |
| US11512604B1 (en) * | 2021-05-04 | 2022-11-29 | Raytheon Technologies Corporation | Spring for radially stacked assemblies |
| US11885498B2 (en) * | 2022-01-31 | 2024-01-30 | General Electric Company | Turbine engine with fuel system including a catalytic reformer |
| US12055058B2 (en) * | 2022-05-31 | 2024-08-06 | Pratt & Whitney Canada Corp. | Joint between gas turbine engine components with a spring element |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL27859C (Direct) * | 1928-12-29 | |||
| GB694651A (en) * | 1950-08-01 | 1953-07-22 | Rolls Royce | Improvements in or relating to turbo-machines |
| FR1095392A (fr) * | 1953-12-01 | 1955-06-01 | Csf | Aubages de turbines à gaz |
| DE2108176A1 (de) * | 1971-02-20 | 1972-08-31 | Motoren Turbinen Union | Befestigung von keramischen Turbinenschaufeln |
| US3857649A (en) * | 1973-08-09 | 1974-12-31 | Westinghouse Electric Corp | Inlet vane structure for turbines |
| USB563412I5 (Direct) | 1975-03-28 | 1976-02-24 |
-
1976
- 1976-02-20 US US05/659,869 patent/US4053257A/en not_active Expired - Lifetime
-
1977
- 1977-01-13 CA CA269,632A patent/CA1042349A/en not_active Expired
- 1977-02-18 JP JP1633977A patent/JPS52115909A/ja active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| US4053257A (en) | 1977-10-11 |
| JPS52115909A (en) | 1977-09-28 |
| JPS564722B2 (Direct) | 1981-01-31 |
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