CH270936A - Turbomachine rotor. - Google Patents
Turbomachine rotor.Info
- Publication number
- CH270936A CH270936A CH270936DA CH270936A CH 270936 A CH270936 A CH 270936A CH 270936D A CH270936D A CH 270936DA CH 270936 A CH270936 A CH 270936A
- Authority
- CH
- Switzerland
- Prior art keywords
- turbomachine rotor
- turbomachine
- rotor
- Prior art date
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
- F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
-
- 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
- F01D5/16—Form or construction for counteracting blade vibration
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB270936X | 1947-02-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH270936A true CH270936A (en) | 1950-09-30 |
Family
ID=10254069
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH270936D CH270936A (en) | 1947-02-17 | 1948-02-12 | Turbomachine rotor. |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH270936A (en) |
FR (1) | FR1059752A (en) |
GB (1) | GB621315A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3917034A1 (en) * | 1988-06-02 | 1989-12-14 | Gen Electric | PROPELLER BLADE FASTENING DEVICE |
US5165856A (en) * | 1988-06-02 | 1992-11-24 | General Electric Company | Fan blade mount |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2819869A (en) * | 1950-05-02 | 1958-01-14 | Jr Andre J Meyer | Mounting arrangement for turbine or compressor blading |
GB741550A (en) * | 1952-07-10 | 1955-12-07 | Havilland Engine Co Ltd | Improvements in or relating to the rotors of multi-stage axial flow compressors or turbines |
BE529656A (en) * | 1953-04-10 | |||
US2919889A (en) * | 1955-03-03 | 1960-01-05 | United Aircraft Corp | Blade mounting |
US2928652A (en) * | 1955-10-12 | 1960-03-15 | Gen Electric | Roll-pin support for turbomachine blades |
DE1025900B (en) * | 1956-10-31 | 1958-03-13 | Gen Electric | Attachment of a turbine blade to the impeller |
US2970809A (en) * | 1958-08-29 | 1961-02-07 | Westinghouse Electric Corp | Blade vibration damping arrangement for elastic fluid machines |
DE1213423B (en) * | 1960-06-04 | 1966-03-31 | Maschf Augsburg Nuernberg Ag | Attachment of the vanes of a guide vane ring of a flow machine to the guide vane carrier by means of rubber-elastic elements |
US3400912A (en) * | 1967-08-16 | 1968-09-10 | United Aircraft Corp | High performance pinned root rotor |
US4480957A (en) * | 1983-04-14 | 1984-11-06 | General Electric Company | Dynamic response modification and stress reduction in dovetail and blade assembly |
US4541778A (en) * | 1984-05-18 | 1985-09-17 | The United States Of America As Represented By The Secretary Of The Navy | Pin rooted blade biaxial air seal |
GB2192237B (en) * | 1986-07-02 | 1990-05-16 | Rolls Royce Plc | Gas turbine engine power turbine |
US5102300A (en) * | 1988-10-07 | 1992-04-07 | United Technologies Corporation | Pinned airfoil propeller assembly |
US5074753A (en) * | 1989-10-16 | 1991-12-24 | Bell Helicopter Textron Inc. | Rotor blade |
US5163817A (en) * | 1989-10-16 | 1992-11-17 | United Technologies Corporation | Rotor blade retention |
US5017092A (en) * | 1989-10-16 | 1991-05-21 | United Technologies Corporation | Rotor blade retention |
US5868351A (en) * | 1996-05-23 | 1999-02-09 | Bell Helicopter Textron Inc. | Rotor blade stowing system |
CN104314619B (en) * | 2014-08-15 | 2016-02-24 | 中国燃气涡轮研究院 | A kind of turbine blisk Natural Frequency of Blade adjust structure and method |
FR3104197B1 (en) * | 2019-12-10 | 2022-07-29 | Safran Aircraft Engines | TURBINE ROTOR WHEEL FOR AN AIRCRAFT TURBOMACHINE |
-
1947
- 1947-02-17 GB GB4588/47A patent/GB621315A/en not_active Expired
-
1948
- 1948-02-12 CH CH270936D patent/CH270936A/en unknown
- 1948-02-16 FR FR1059752D patent/FR1059752A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3917034A1 (en) * | 1988-06-02 | 1989-12-14 | Gen Electric | PROPELLER BLADE FASTENING DEVICE |
US5102302A (en) * | 1988-06-02 | 1992-04-07 | General Electric Company | Fan blade mount |
US5165856A (en) * | 1988-06-02 | 1992-11-24 | General Electric Company | Fan blade mount |
DE3917034C2 (en) * | 1988-06-02 | 1998-06-04 | Gen Electric | Propeller blade fastening device |
Also Published As
Publication number | Publication date |
---|---|
GB621315A (en) | 1949-04-07 |
FR1059752A (en) | 1954-03-29 |
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