GB532372A - Improvements in and relating to elastic fluid turbines - Google Patents
Improvements in and relating to elastic fluid turbinesInfo
- Publication number
- GB532372A GB532372A GB24706/39A GB2470639A GB532372A GB 532372 A GB532372 A GB 532372A GB 24706/39 A GB24706/39 A GB 24706/39A GB 2470639 A GB2470639 A GB 2470639A GB 532372 A GB532372 A GB 532372A
- Authority
- GB
- United Kingdom
- Prior art keywords
- elastic fluid
- fluid turbines
- relating
- roots
- aug
- 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
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
532,372. Elastic fluid turbines. BRITISH THOMSON-HOUSTON CO., Ltd. Aug. 28, 1938, No. 24706. Convention date, Aug. 27, 1938. [Class 110 (iii)] The meeting faces of the roots and the cover poitions have inter-engaging parts which extend parallel to the rotor axis. Holes 24, 25, lying equally in adjacent coverportions and roots, may be drilled after assembly and be filled with .pins the ends of which are riveted over, or secured by peening over the ends of the holes. Or, inter-fitting tongues and grooves may be formed in the meeting faces.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US532372XA | 1938-08-27 | 1938-08-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB532372A true GB532372A (en) | 1941-01-22 |
Family
ID=21982821
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24706/39A Expired GB532372A (en) | 1938-08-27 | 1939-08-28 | Improvements in and relating to elastic fluid turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB532372A (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2805838A (en) * | 1950-06-22 | 1957-09-10 | Power Jets Res & Dev Ltd | Rotors for turbines and similarly bladed fluid flow machines |
US3051440A (en) * | 1959-07-27 | 1962-08-28 | Rotax Ltd | Air driven turbines |
US4781532A (en) * | 1985-06-28 | 1988-11-01 | Bbc Brown, Boveri & Company, Ltd. | Blade retention feature for saddle fir tree root blades of turbo machines and method of using same |
US5441385A (en) * | 1993-12-13 | 1995-08-15 | Solar Turbines Incorporated | Turbine nozzle/nozzle support structure |
EP1408199A1 (en) * | 2002-10-08 | 2004-04-14 | United Technologies Corporation | Leak resistant vane cluster |
EP1512838A3 (en) * | 2003-09-02 | 2006-07-19 | Man Turbo Ag | Rotor for a steam or gas turbine |
US7252481B2 (en) * | 2004-05-14 | 2007-08-07 | Pratt & Whitney Canada Corp. | Natural frequency tuning of gas turbine engine blades |
EP1873355A1 (en) * | 2006-06-27 | 2008-01-02 | Siemens Aktiengesellschaft | Turbine rotor blade |
EP2612996A1 (en) * | 2012-01-04 | 2013-07-10 | General Electric Company | Device and method for aligning tip shrouds |
JP2014066223A (en) * | 2012-09-27 | 2014-04-17 | Mitsubishi Heavy Ind Ltd | Turbine stationary blade vibration control structure |
EP2803821A1 (en) * | 2013-05-13 | 2014-11-19 | Siemens Aktiengesellschaft | Blade device, blade system, and corresponding method of manufacturing a blade system |
EP2562355A3 (en) * | 2011-08-23 | 2018-04-11 | General Electric Company | Coupled blade platforms and methods of sealing |
-
1939
- 1939-08-28 GB GB24706/39A patent/GB532372A/en not_active Expired
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2805838A (en) * | 1950-06-22 | 1957-09-10 | Power Jets Res & Dev Ltd | Rotors for turbines and similarly bladed fluid flow machines |
US3051440A (en) * | 1959-07-27 | 1962-08-28 | Rotax Ltd | Air driven turbines |
US4781532A (en) * | 1985-06-28 | 1988-11-01 | Bbc Brown, Boveri & Company, Ltd. | Blade retention feature for saddle fir tree root blades of turbo machines and method of using same |
US5441385A (en) * | 1993-12-13 | 1995-08-15 | Solar Turbines Incorporated | Turbine nozzle/nozzle support structure |
US5591003A (en) * | 1993-12-13 | 1997-01-07 | Solar Turbines Incorporated | Turbine nozzle/nozzle support structure |
WO2004033871A3 (en) * | 2002-10-08 | 2009-04-23 | United Technologies Corp | Leak resistant vane cluster |
WO2004033871A2 (en) * | 2002-10-08 | 2004-04-22 | United Technologies Corporation | Leak resistant vane cluster |
US6910854B2 (en) | 2002-10-08 | 2005-06-28 | United Technologies Corporation | Leak resistant vane cluster |
EP1408199A1 (en) * | 2002-10-08 | 2004-04-14 | United Technologies Corporation | Leak resistant vane cluster |
EP1512838A3 (en) * | 2003-09-02 | 2006-07-19 | Man Turbo Ag | Rotor for a steam or gas turbine |
US7104758B2 (en) | 2003-09-02 | 2006-09-12 | Man Turbo Ag | Rotor of a steam or gas turbine |
US7252481B2 (en) * | 2004-05-14 | 2007-08-07 | Pratt & Whitney Canada Corp. | Natural frequency tuning of gas turbine engine blades |
EP1873355A1 (en) * | 2006-06-27 | 2008-01-02 | Siemens Aktiengesellschaft | Turbine rotor blade |
EP2562355A3 (en) * | 2011-08-23 | 2018-04-11 | General Electric Company | Coupled blade platforms and methods of sealing |
EP2612996A1 (en) * | 2012-01-04 | 2013-07-10 | General Electric Company | Device and method for aligning tip shrouds |
JP2014066223A (en) * | 2012-09-27 | 2014-04-17 | Mitsubishi Heavy Ind Ltd | Turbine stationary blade vibration control structure |
EP2803821A1 (en) * | 2013-05-13 | 2014-11-19 | Siemens Aktiengesellschaft | Blade device, blade system, and corresponding method of manufacturing a blade system |
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