GB850507A - Compressor or turbine rotors having shrouded blades - Google Patents
Compressor or turbine rotors having shrouded bladesInfo
- Publication number
- GB850507A GB850507A GB8146/59A GB814659A GB850507A GB 850507 A GB850507 A GB 850507A GB 8146/59 A GB8146/59 A GB 8146/59A GB 814659 A GB814659 A GB 814659A GB 850507 A GB850507 A GB 850507A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shroud
- blade
- brazed
- ring
- rings
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
850,507. Compressor and turbine rotor blades. GENERAL MOTORS CORPORATION. March 9, 1959 [June 11, 1958], No. 8146/59. Class 110 (3). A compressor or turbine rotor having a blade tip shroud comprises inner and outer sheetmetal rings brazed or welded together forming a circumferential channel receiving a tang on each blade tip, the tangs projecting through holes in the shroud and being secured thereto by a pin or rivet. In Fig. 3, a shroud ring 27 consists of an inner ring 28 and a generally " W "-shaped outer ring 29 brazed or welded to ring 28. A tang 32 integral with the blade 26 extends through an opening 33 in the shroud ring which also includes, at each blade position an attachment block 34 brazed to the rings 28 and 29 to provide a rigid attachment for the blade. To lock the tang, a longitudinally split pin 38 is inserted in holes drilled in the outer ring 29 and attachment block 34. In another embodiment (Fig. 8) the blade 51 has two spaced tangs 52 at its tip, which project, through openings 64 in the inner ring 54, into the outer ring 56. Three attachment blocks 61 are brazed within the channels 57, 58, 59 and a pin 66 is inserted through the coaxial holes 62 and 63 to secure the tangs to the shroud. In a further embodiment (Fig. 14), the blade 71 has a single tang 72 attached by rivets 83 to two attachment strips 78 on either side of it. The attachment strips are brazed or welded to the shroud which comprises an inner ring 74 welded to two L-shaped rings 76 and an intermediate ring 77 in segments extending between the blades. In the final embodiment (Fig. 17), the shroud 92 comprises an inner ring 93 and a generally W "- shaped outer ring 94 brazed or welded together. Also brazed to the outer ring on each side of two openings in the rings 93 and 94 are attachmentblocks 96, which enclose the two tangs 98 of blade 91. Pins 101 secure the tangs to the shroud, and may be rivets, as shown, or split tubes, or headed pins retained by snap-rings.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US850507XA | 1958-06-11 | 1958-06-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB850507A true GB850507A (en) | 1960-10-05 |
Family
ID=22189145
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8146/59A Expired GB850507A (en) | 1958-06-11 | 1959-03-09 | Compressor or turbine rotors having shrouded blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB850507A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140010643A1 (en) * | 2011-03-11 | 2014-01-09 | Alstom Technology Ltd. | Method of fabricating a steam turbine deflector |
WO2014137441A1 (en) * | 2012-12-21 | 2014-09-12 | General Electric Company | Rotor blade and corresponding manufacturing method |
CN114991877A (en) * | 2022-08-03 | 2022-09-02 | 成都中科翼能科技有限公司 | Combined blade structure of turbine rotor |
-
1959
- 1959-03-09 GB GB8146/59A patent/GB850507A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140010643A1 (en) * | 2011-03-11 | 2014-01-09 | Alstom Technology Ltd. | Method of fabricating a steam turbine deflector |
US9604323B2 (en) * | 2011-03-11 | 2017-03-28 | General Electric Technology Gmbh | Method of fabricating a steam turbine deflector |
WO2014137441A1 (en) * | 2012-12-21 | 2014-09-12 | General Electric Company | Rotor blade and corresponding manufacturing method |
CN114991877A (en) * | 2022-08-03 | 2022-09-02 | 成都中科翼能科技有限公司 | Combined blade structure of turbine rotor |
CN114991877B (en) * | 2022-08-03 | 2022-11-18 | 成都中科翼能科技有限公司 | Combined blade structure of turbine rotor |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB715145A (en) | Improvements in or relating to stator constructions for compressors | |
GB1286776A (en) | Bladed rotors for turbomachines | |
GB1467374A (en) | Hollow turbomachinery blades | |
GB742194A (en) | Improvements in or relating to rotors for compressors and turbines | |
GB1208507A (en) | Blade fixing arrangement | |
GB1491556A (en) | Rotor blades for turbomachines | |
GB1270203A (en) | Improvements in turbo machines | |
GB1095830A (en) | Bladed rotor for a fluid flow machine such as a gas turbine engine | |
GB827264A (en) | Improvements in compressor rotor | |
GB751128A (en) | Improvements in turbine or compressor blades | |
GB1353114A (en) | Turbo-machinery | |
GB1053420A (en) | ||
GB701263A (en) | Improvements in or relating to turbo-machines | |
GB850507A (en) | Compressor or turbine rotors having shrouded blades | |
GB980656A (en) | Improvements in and relating to turbines and like machines | |
GB967940A (en) | Improvements in turbine or compressor nozzle and vane assembly | |
GB1331711A (en) | Turbomachine rotor blade retaining means | |
GB1102219A (en) | Bladed turbine or compressor rotors | |
GB1236366A (en) | Elastic fluid machine | |
GB954323A (en) | Improvements in or relating to bladed rotors for fluid flow machines such as turbines | |
GB1177779A (en) | Blade Lock | |
GB904546A (en) | Improvements in or relating to rotor blades of turbines and compressors | |
GB980337A (en) | Improvements in or relating to a rotor for a compressor turbine or like bladed fluidflow machine | |
GB1012899A (en) | Air cooled gas turbine blades | |
GB846623A (en) | A stator casing and blade assembly for an axial flow compressor |