CA975302A - Turbine rotor having cushioned support surfaces for ceramic blades mounted thereon - Google Patents
Turbine rotor having cushioned support surfaces for ceramic blades mounted thereonInfo
- Publication number
- CA975302A CA975302A CA194,854A CA194854A CA975302A CA 975302 A CA975302 A CA 975302A CA 194854 A CA194854 A CA 194854A CA 975302 A CA975302 A CA 975302A
- Authority
- CA
- Canada
- Prior art keywords
- turbine rotor
- support surfaces
- blades mounted
- cushioned support
- ceramic 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3084—Fixing blades to rotors; Blade roots ; Blade spacers the blades being made of ceramics
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US00345391A US3809495A (en) | 1973-03-27 | 1973-03-27 | Turbine rotor having cushioned support surfaces for ceramic blades mounted thereon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA975302A true CA975302A (en) | 1975-09-30 |
Family
ID=23354858
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA194,854A Expired CA975302A (en) | 1973-03-27 | 1974-03-13 | Turbine rotor having cushioned support surfaces for ceramic blades mounted thereon |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US3809495A (de) |
| CA (1) | CA975302A (de) |
| CH (1) | CH576066A5 (de) |
| DE (1) | DE2411992C2 (de) |
| FR (1) | FR2223546B1 (de) |
| GB (1) | GB1438238A (de) |
| IT (1) | IT1009669B (de) |
| NL (1) | NL7403268A (de) |
| SE (1) | SE391962B (de) |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3891351A (en) * | 1974-03-25 | 1975-06-24 | Theodore J Norbut | Turbine disc |
| US4480957A (en) * | 1983-04-14 | 1984-11-06 | General Electric Company | Dynamic response modification and stress reduction in dovetail and blade assembly |
| US4491421A (en) * | 1983-11-21 | 1985-01-01 | De Dietrich (Usa), Inc. | Impeller assembly and shaft having interference fit |
| US4508455A (en) * | 1983-11-21 | 1985-04-02 | De Dietrich (Usa), Inc. | Agitator including impeller assembly and shaft having interference fit |
| US4820126A (en) * | 1988-02-22 | 1989-04-11 | Westinghouse Electric Corp. | Turbomachine rotor assembly having reduced stress concentrations |
| US6132175A (en) * | 1997-05-29 | 2000-10-17 | Alliedsignal, Inc. | Compliant sleeve for ceramic turbine blades |
| US6409473B1 (en) | 2000-06-27 | 2002-06-25 | Honeywell International, Inc. | Low stress connection methodology for thermally incompatible materials |
| EP1561905A1 (de) * | 2004-02-09 | 2005-08-10 | Siemens Aktiengesellschaft | Plastisch deformierbare Schicht im Verbindungsbereich einer Turbinenschaufel und Verfahren zur Schaufelbefestigung |
| GB0403064D0 (en) * | 2004-02-12 | 2004-03-17 | Rolls Royce Plc | Gas turbine engine rotor blade, rotor disc and bladed disc assembly, and a bearing arrangement for reducing the effects of dynamic contact stresses |
| US7306434B2 (en) * | 2004-02-12 | 2007-12-11 | Rolls-Royce Plc | Reduction of co-efficient of friction to reduce stress ratio in bearings and gas turbine parts |
| US8210819B2 (en) * | 2008-02-22 | 2012-07-03 | Siemens Energy, Inc. | Airfoil structure shim |
| GB0911459D0 (en) * | 2009-07-02 | 2009-08-12 | Rolls Royce Plc | An assembly providing contaminant removal |
| US8550776B2 (en) * | 2010-07-28 | 2013-10-08 | General Electric Company | Composite vane mounting |
| US8734101B2 (en) * | 2010-08-31 | 2014-05-27 | General Electric Co. | Composite vane mounting |
| GB201106278D0 (en) * | 2011-04-14 | 2011-05-25 | Rolls Royce Plc | Annulus filler system |
| EP2832957A1 (de) * | 2013-07-31 | 2015-02-04 | ALSTOM Technology Ltd | Rotor mit Nut mit nachgiebiger Schicht |
| US11021972B2 (en) * | 2018-08-14 | 2021-06-01 | Rolls-Royce North American Technologies Inc. | Variable pitch blade holder for gas turbine engine |
| DE102021120876A1 (de) | 2021-08-11 | 2023-02-16 | MTU Aero Engines AG | Schaufelfussaufnahme zum aufnehmen einer laufschaufel |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB280221A (en) * | 1926-11-06 | 1928-02-23 | Alfred Buechi | Improvements in blading for gas and steam turbines |
| US2317338A (en) * | 1942-02-07 | 1943-04-20 | Westinghouse Electric & Mfg Co | Turbine blade fastening apparatus |
| US2595829A (en) * | 1946-12-19 | 1952-05-06 | Benson Mfg Company | Axial flow fan and compressor |
| GB664986A (en) * | 1948-10-29 | 1952-01-16 | Maschf Augsburg Nuernberg Ag | Ceramic blade for turbines |
| DE1025421B (de) * | 1955-10-31 | 1958-03-06 | Maschf Augsburg Nuernberg Ag | Befestigung von Lauftschaufeln sproeden Werkstoffes in metallischem Schaufeltraeger |
| DE1045730B (de) * | 1957-12-18 | 1958-12-04 | Maschf Augsburg Nuernberg Ag | Einrichtung an metallischen Schaufeltraegern zur Befestigung von Laufschaufeln aus sproeden Werkstoffen, insbesondere fuer Gasturbinen |
| US3313519A (en) * | 1965-06-22 | 1967-04-11 | Ass Elect Ind | Turbine rotors |
-
1973
- 1973-03-27 US US00345391A patent/US3809495A/en not_active Expired - Lifetime
-
1974
- 1974-03-12 NL NL7403268A patent/NL7403268A/xx not_active Application Discontinuation
- 1974-03-13 DE DE2411992A patent/DE2411992C2/de not_active Expired
- 1974-03-13 CA CA194,854A patent/CA975302A/en not_active Expired
- 1974-03-18 GB GB1190674A patent/GB1438238A/en not_active Expired
- 1974-03-19 SE SE7403718A patent/SE391962B/xx unknown
- 1974-03-20 CH CH386174A patent/CH576066A5/xx not_active IP Right Cessation
- 1974-03-26 FR FR7410266A patent/FR2223546B1/fr not_active Expired
- 1974-04-08 IT IT20707/74A patent/IT1009669B/it active
Also Published As
| Publication number | Publication date |
|---|---|
| IT1009669B (it) | 1976-12-20 |
| DE2411992A1 (de) | 1974-10-03 |
| FR2223546B1 (de) | 1978-11-10 |
| DE2411992C2 (de) | 1982-07-15 |
| NL7403268A (de) | 1974-10-01 |
| FR2223546A1 (de) | 1974-10-25 |
| US3809495A (en) | 1974-05-07 |
| SE391962B (sv) | 1977-03-07 |
| GB1438238A (en) | 1976-06-03 |
| CH576066A5 (de) | 1976-05-31 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA975302A (en) | Turbine rotor having cushioned support surfaces for ceramic blades mounted thereon | |
| CA1001952A (en) | Fluid cooled turbine rotor blade | |
| CA995140A (en) | Cooled turbine blade ring assembly | |
| CA995141A (en) | Inlet vane structure for turbines | |
| CA984361A (en) | Rotor blade retention system | |
| CA975300A (en) | Axial flow turbine structure | |
| CA962601A (en) | Turbine rotor | |
| CA979810A (en) | Cooled rotor blade for a gas turbine | |
| CA962254A (en) | Helicopter rotor blade | |
| CA923043A (en) | Rotor blade structure | |
| CA1030339A (en) | Blade mounting assemblies | |
| CA1002781A (en) | Turbine meter with conical rotor | |
| CA998614A (en) | Rotor assemblies | |
| AU6351373A (en) | Hacksaw with novel blade mounting means | |
| CA1016524A (en) | Helicopter rotor blade | |
| HK12877A (en) | Airfoil rotor for toy helicopter | |
| CA988310A (en) | Turbine by-pass arrangement for thermal power plants | |
| CA1003757A (en) | Nozzle structure for steam turbines | |
| CA988906A (en) | Helicopter blade | |
| CA1010005A (en) | Rotor means for an aircraft | |
| SU574542A1 (ru) | Опора турбины | |
| CA1002972A (en) | Shaft mounting means | |
| CA991085A (en) | Temperature control for turbine rotor cavity | |
| CA1001555A (en) | Rotor blades | |
| CA1014358A (en) | Turbo-machine plant having optional operating modes |