GB621315A - Improvements relating to compressors and turbines - Google Patents
Improvements relating to compressors and turbinesInfo
- Publication number
- GB621315A GB621315A GB4588/47A GB458847A GB621315A GB 621315 A GB621315 A GB 621315A GB 4588/47 A GB4588/47 A GB 4588/47A GB 458847 A GB458847 A GB 458847A GB 621315 A GB621315 A GB 621315A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- compressors
- blades
- lugs
- turbines
- 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
- F01D5/3053—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 |
---|---|
GB621315A true GB621315A (en) | 1949-04-07 |
Family
ID=10254069
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4588/47A Expired GB621315A (en) | 1947-02-17 | 1947-02-17 | Improvements relating to compressors and turbines |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH270936A (fr) |
FR (1) | FR1059752A (fr) |
GB (1) | GB621315A (fr) |
Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2795393A (en) * | 1952-07-10 | 1957-06-11 | Havilland Engine Co Ltd | Rotors of multi-stage axial flow compressors or turbines |
US2819869A (en) * | 1950-05-02 | 1958-01-14 | Jr Andre J Meyer | Mounting arrangement for turbine or compressor blading |
DE1025900B (de) * | 1956-10-31 | 1958-03-13 | Gen Electric | Befestigung einer Turbinenschaufel am Laufrad |
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 |
US2970809A (en) * | 1958-08-29 | 1961-02-07 | Westinghouse Electric Corp | Blade vibration damping arrangement for elastic fluid machines |
US2980395A (en) * | 1953-04-10 | 1961-04-18 | Rolls Royce | Rotor with pivoted blades for compressors and turbines |
DE1213423B (de) * | 1960-06-04 | 1966-03-31 | Maschf Augsburg Nuernberg Ag | Befestigung der Schaufeln eines Leitschaufel-kranzes einer Stroemungsmaschine am Leitschaufeltraeger mittels gummielastischer Elemente |
US3400912A (en) * | 1967-08-16 | 1968-09-10 | United Aircraft Corp | High performance pinned root rotor |
FR2544381A1 (fr) * | 1983-04-14 | 1984-10-19 | Gen Electric | Composant tournant comprenant des aubes a queue d'aronde modifiee |
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 |
FR2601068A1 (fr) * | 1986-07-02 | 1988-01-08 | Rolls Royce Plc | Turbine de puissance pour moteur a turbine a gaz. |
WO1991005700A1 (fr) * | 1989-10-16 | 1991-05-02 | Bell Helicopter Textron Inc. | Pale de rotor |
US5017092A (en) * | 1989-10-16 | 1991-05-21 | United Technologies Corporation | Rotor blade retention |
US5102300A (en) * | 1988-10-07 | 1992-04-07 | United Technologies Corporation | Pinned airfoil propeller assembly |
US5102302A (en) * | 1988-06-02 | 1992-04-07 | General Electric Company | Fan blade mount |
US5163817A (en) * | 1989-10-16 | 1992-11-17 | United Technologies Corporation | Rotor blade retention |
US5165856A (en) * | 1988-06-02 | 1992-11-24 | General Electric Company | Fan blade mount |
US5868351A (en) * | 1996-05-23 | 1999-02-09 | Bell Helicopter Textron Inc. | Rotor blade stowing system |
CN104314619A (zh) * | 2014-08-15 | 2015-01-28 | 中国燃气涡轮研究院 | 一种涡轮整体叶盘叶片固有频率调整结构及方法 |
US20220412216A1 (en) * | 2019-12-10 | 2022-12-29 | 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/de unknown
- 1948-02-16 FR FR1059752D patent/FR1059752A/fr not_active Expired
Cited By (25)
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 |
US2795393A (en) * | 1952-07-10 | 1957-06-11 | Havilland Engine Co Ltd | Rotors of multi-stage axial flow compressors or turbines |
US2980395A (en) * | 1953-04-10 | 1961-04-18 | Rolls Royce | Rotor with pivoted blades for compressors and turbines |
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 (de) * | 1956-10-31 | 1958-03-13 | Gen Electric | Befestigung einer Turbinenschaufel am Laufrad |
US2970809A (en) * | 1958-08-29 | 1961-02-07 | Westinghouse Electric Corp | Blade vibration damping arrangement for elastic fluid machines |
DE1213423B (de) * | 1960-06-04 | 1966-03-31 | Maschf Augsburg Nuernberg Ag | Befestigung der Schaufeln eines Leitschaufel-kranzes einer Stroemungsmaschine am Leitschaufeltraeger mittels gummielastischer Elemente |
US3400912A (en) * | 1967-08-16 | 1968-09-10 | United Aircraft Corp | High performance pinned root rotor |
FR2544381A1 (fr) * | 1983-04-14 | 1984-10-19 | Gen Electric | Composant tournant comprenant des aubes a queue d'aronde modifiee |
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 |
FR2601068A1 (fr) * | 1986-07-02 | 1988-01-08 | Rolls Royce Plc | Turbine de puissance pour moteur a turbine a gaz. |
US5165856A (en) * | 1988-06-02 | 1992-11-24 | General Electric Company | Fan blade mount |
US5102302A (en) * | 1988-06-02 | 1992-04-07 | General Electric Company | Fan blade mount |
US5354176A (en) * | 1988-06-02 | 1994-10-11 | General Electric Company | Fan blade mount |
US5102300A (en) * | 1988-10-07 | 1992-04-07 | United Technologies Corporation | Pinned airfoil propeller assembly |
US5017092A (en) * | 1989-10-16 | 1991-05-21 | United Technologies Corporation | Rotor blade retention |
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 |
WO1991005700A1 (fr) * | 1989-10-16 | 1991-05-02 | Bell Helicopter Textron Inc. | Pale de rotor |
US5868351A (en) * | 1996-05-23 | 1999-02-09 | Bell Helicopter Textron Inc. | Rotor blade stowing system |
CN104314619A (zh) * | 2014-08-15 | 2015-01-28 | 中国燃气涡轮研究院 | 一种涡轮整体叶盘叶片固有频率调整结构及方法 |
CN104314619B (zh) * | 2014-08-15 | 2016-02-24 | 中国燃气涡轮研究院 | 一种涡轮整体叶盘叶片固有频率调整结构及方法 |
US20220412216A1 (en) * | 2019-12-10 | 2022-12-29 | Safran Aircraft Engines | Turbine rotor wheel for an aircraft turbomachine |
US11788423B2 (en) * | 2019-12-10 | 2023-10-17 | Safran Aircraft Engines | Turbine rotor wheel for an aircraft turbomachine |
Also Published As
Publication number | Publication date |
---|---|
CH270936A (de) | 1950-09-30 |
FR1059752A (fr) | 1954-03-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB621315A (en) | Improvements relating to compressors and turbines | |
GB599391A (en) | Improvements in and relating to axial flow compressors, turbines and the like machines | |
GB608514A (en) | Improvements in or relating to drum structures | |
GB733918A (en) | Improvements in blades of elastic fluid turbines and dynamic compressors | |
GB621551A (en) | Improvements in or relating to axial-flow compressors and turbines | |
GB902064A (en) | Blade damping means for compressors and turbines | |
GB712589A (en) | Improvements in or relating to guide vane assemblies in annular fluid ducts | |
GB586560A (en) | Improvements in axial flow compressors and like machines | |
GB630277A (en) | Improvements relating to axial-flow compressors | |
GB1231424A (fr) | ||
GB622767A (en) | Improvements in or relating to the blades of axial flow compressors and turbines andthe means for fixing them | |
GB1509185A (en) | Fluid driven turbo machines | |
GB732622A (en) | Oscillation dampers for the blades of steam and gas turbines, axial flow compressors and similar machines | |
GB590141A (en) | Improvements in and relating to variable pitch fans, axial flow compressors and the like | |
GB624777A (en) | Improvements in or relating to stator casings for compressors and like machines | |
GB711528A (en) | Elastic fluid turbine plant | |
GB732920A (en) | Improvements relating to blade assemblies of turbo-machines such as compressors and turbines | |
GB777835A (en) | Improvements in or relating to stator structures for turbines or compressors of gas turbine engines | |
GB600057A (en) | Improvements in or relating to the mounting of blades in axial flow compressors, turbines, or the like | |
GB628102A (en) | Improvements in or relating to stator structures of turbines and similar fluid flow machines | |
GB586564A (en) | Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus | |
GB600025A (en) | Improvements in and relating to casings for turbines, compressors and the like | |
GB646728A (en) | Improvements in or relating to stator casings for turbines, compressors and like rotary bladed fluid flow machines | |
GB641144A (en) | Improvements in or relating to blade-fixing means for compressors, fans, turbines orthe like | |
GB615219A (en) | Improvements relating to rotary power conversion machines |