GB640532A - Improvements in and relating to elastic fluid turbines - Google Patents
Improvements in and relating to elastic fluid turbinesInfo
- Publication number
- GB640532A GB640532A GB31338/47A GB3133847A GB640532A GB 640532 A GB640532 A GB 640532A GB 31338/47 A GB31338/47 A GB 31338/47A GB 3133847 A GB3133847 A GB 3133847A GB 640532 A GB640532 A GB 640532A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fluid turbines
- blade groove
- relating
- elastic fluid
- rotor
- 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
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
- F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60C—VEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
- B60C13/00—Tyre sidewalls; Protecting, decorating, marking, or the like, thereof
- B60C13/02—Arrangement of grooves or ribs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/40—Alighting gear characterised by elements which contact the ground or similar surface the elements being rotated before touch-down
-
- 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
- F01D5/32—Locking, e.g. by final locking blades or keys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60C—VEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
- B60C2200/00—Tyres specially adapted for particular applications
- B60C2200/02—Tyres specially adapted for particular applications for aircrafts
Abstract
640,532. Elastic-fluid turbines. BRITISH THOMSON-HOUSTON CO., Ltd., and JOHNSON, J. W. Nov. 26. 1947. No. 31338. [Class 110(iii)]. The gap by which turbine blade roots are introduced to the annular blade groove in the rotor is closed by a block b of dovetailed c r o s s-section held in place by a second piece c. The parts b, c are assembled as shown prior to the machining of the sides of the rotor blade groove. The part c is then withdrawn and the part b moved back from the blade groove. When the blades are in position, the part c is re-inserted and secured by grub screws d.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US731789A US2439033A (en) | 1947-03-01 | 1947-03-01 | Vaned tire |
GB31338/47A GB640532A (en) | 1947-11-26 | 1947-11-26 | Improvements in and relating to elastic fluid turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB31338/47A GB640532A (en) | 1947-11-26 | 1947-11-26 | Improvements in and relating to elastic fluid turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB640532A true GB640532A (en) | 1950-07-19 |
Family
ID=10321644
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB31338/47A Expired GB640532A (en) | 1947-03-01 | 1947-11-26 | Improvements in and relating to elastic fluid turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB640532A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10012381A1 (en) * | 2000-03-14 | 2001-09-20 | Man Turbomasch Ag Ghh Borsig | Bucket lock and method for manufacturing a paddle lock |
DE102008048261A1 (en) * | 2008-09-22 | 2010-04-01 | Siemens Aktiengesellschaft | Axial turbomachinery rotor with a paddle lock and method of making the same |
-
1947
- 1947-11-26 GB GB31338/47A patent/GB640532A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10012381A1 (en) * | 2000-03-14 | 2001-09-20 | Man Turbomasch Ag Ghh Borsig | Bucket lock and method for manufacturing a paddle lock |
US6431836B2 (en) | 2000-03-14 | 2002-08-13 | Man Turbomaschinen Ag Ghh Borsig | Blade lock and process for manufacturing a blade lock |
EP1134359A3 (en) * | 2000-03-14 | 2003-07-30 | MAN Turbomaschinen AG | Blade lock and method to make such a blade lock |
CZ297759B6 (en) * | 2000-03-14 | 2007-03-21 | Man Turbo Ag | Blade lock and process for producing thereof |
DE102008048261A1 (en) * | 2008-09-22 | 2010-04-01 | Siemens Aktiengesellschaft | Axial turbomachinery rotor with a paddle lock and method of making the same |
DE102008048261B4 (en) * | 2008-09-22 | 2017-04-06 | Siemens Aktiengesellschaft | Axial turbomachinery rotor with a paddle lock and method of making the same |
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