GB260411A - Improvements relating to turbines - Google Patents
Improvements relating to turbinesInfo
- Publication number
- GB260411A GB260411A GB2554725A GB2554725A GB260411A GB 260411 A GB260411 A GB 260411A GB 2554725 A GB2554725 A GB 2554725A GB 2554725 A GB2554725 A GB 2554725A GB 260411 A GB260411 A GB 260411A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- gravity
- rotation
- action
- blades
- 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
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
260,411. Walker, G. W. Higgs-, and Pretropolitan-Vickers Electrical Co., Ltd. Oct. 13, 1925. Blades.-To enable long blades to be used at high peripheral speeds, the effective portion of the blade is inclined in the direction of rotation sufficiently to cause the locus 0 G of the centres of gravity of successive transverse sections of the blade from end to end thereof to lie in advance, in the direction of rotation, of a line 0 R drawn radially of the turbine rotor through the centre of gravity 0 of the section at the root of the blade. Preferably the angle between the lines 0 G, 0 R is such that the tensile stresses at the thin edges of the concave side of the blade due to blending action by the steam are neutralized by those due to the action of centrifugal force at these parts at the normal speed of the rotor.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2554725A GB260411A (en) | 1925-10-13 | 1925-10-13 | Improvements relating to turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2554725A GB260411A (en) | 1925-10-13 | 1925-10-13 | Improvements relating to turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB260411A true GB260411A (en) | 1926-11-04 |
Family
ID=10229448
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2554725A Expired GB260411A (en) | 1925-10-13 | 1925-10-13 | Improvements relating to turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB260411A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0570106A1 (en) * | 1992-05-15 | 1993-11-18 | Gec Alsthom Limited | Turbine blade assembly |
EP1524406A1 (en) * | 2003-10-16 | 2005-04-20 | Snecma Moteurs | Configuration of a turbomachine rotor blade |
US20170159461A1 (en) * | 2015-12-03 | 2017-06-08 | MTU Aero Engines AG | Stacking of rotor blades on centroids |
CN113513368A (en) * | 2021-07-08 | 2021-10-19 | 哈尔滨工程大学 | Turbine capable of directly backing with primary and secondary moving blade structures |
-
1925
- 1925-10-13 GB GB2554725A patent/GB260411A/en not_active Expired
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0570106A1 (en) * | 1992-05-15 | 1993-11-18 | Gec Alsthom Limited | Turbine blade assembly |
US5575620A (en) * | 1992-05-15 | 1996-11-19 | Gec Alsthom Limited | Turbine blade assembly |
EP1524406A1 (en) * | 2003-10-16 | 2005-04-20 | Snecma Moteurs | Configuration of a turbomachine rotor blade |
FR2861128A1 (en) * | 2003-10-16 | 2005-04-22 | Snecma Moteurs | DEVICE FOR ATTACHING A MOBILE DARK TO A TURBINE ROTOR DISK IN A TURBOMACHINE |
US7326035B2 (en) | 2003-10-16 | 2008-02-05 | Snecma Moteurs | Device for attaching a moving blade to a turbine rotor disk in a turbomachine |
CN100453772C (en) * | 2003-10-16 | 2009-01-21 | 斯奈克玛公司 | Apparatus for mounting blade on turbine rotor plate in turbo machine |
US20170159461A1 (en) * | 2015-12-03 | 2017-06-08 | MTU Aero Engines AG | Stacking of rotor blades on centroids |
US11125088B2 (en) | 2015-12-03 | 2021-09-21 | MTU Aero Engines AG | Stacking of rotor blades on centroids |
CN113513368A (en) * | 2021-07-08 | 2021-10-19 | 哈尔滨工程大学 | Turbine capable of directly backing with primary and secondary moving blade structures |
CN113513368B (en) * | 2021-07-08 | 2022-09-02 | 哈尔滨工程大学 | Turbine capable of directly backing with primary and secondary moving blade structures |
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