GB179920A - Improved means for securing blades to turbine rotors - Google Patents
Improved means for securing blades to turbine rotorsInfo
- Publication number
- GB179920A GB179920A GB11585/22A GB1158522A GB179920A GB 179920 A GB179920 A GB 179920A GB 11585/22 A GB11585/22 A GB 11585/22A GB 1158522 A GB1158522 A GB 1158522A GB 179920 A GB179920 A GB 179920A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- blades
- improved means
- turbine rotors
- pins
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
179,920. Metropolitan-Vickers Electrical Co., Ltd., (Assignees of Herr, H. T.). May 10, 1921, [Convention date]. Blades.-Blades 13 are secured to a turbine disc rotor 15 by means of pins 20 inclined to the axis of the rotor and with their axes intersecting the rotor axis. The pins 20 are preferably tapered and their inner ends are arranged so that their line clears the root of the adjacent blade ring. The inner shank of a blade bears against a shallow flange 17 on the rotor.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US468412A US1452602A (en) | 1921-05-10 | 1921-05-10 | Turbine-blade fastening |
Publications (1)
Publication Number | Publication Date |
---|---|
GB179920A true GB179920A (en) | 1922-09-07 |
Family
ID=23859708
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB11585/22A Expired GB179920A (en) | 1921-05-10 | 1922-04-25 | Improved means for securing blades to turbine rotors |
Country Status (2)
Country | Link |
---|---|
US (1) | US1452602A (en) |
GB (1) | GB179920A (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2651494A (en) * | 1949-11-24 | 1953-09-08 | Svenska Flygmotor Aktiebolaget | Turbine disk |
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 |
US2921769A (en) * | 1953-06-08 | 1960-01-19 | Peerless Turbine Corp | Turbine rotor |
US3694104A (en) * | 1970-10-07 | 1972-09-26 | Garrett Corp | Turbomachinery blade |
JP5538468B2 (en) * | 2012-03-30 | 2014-07-02 | 株式会社日立製作所 | Method of machining pin joint of turbine rotor blade and turbine rotor, and turbine rotor blade |
US9784116B2 (en) | 2015-01-15 | 2017-10-10 | General Electric Company | Turbine shroud assembly |
-
1921
- 1921-05-10 US US468412A patent/US1452602A/en not_active Expired - Lifetime
-
1922
- 1922-04-25 GB GB11585/22A patent/GB179920A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US1452602A (en) | 1923-04-24 |
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