GB195050A - Improvements in steam turbine blades, and in the method of manufacturing such blades - Google Patents
Improvements in steam turbine blades, and in the method of manufacturing such bladesInfo
- Publication number
- GB195050A GB195050A GB5356/23A GB535623A GB195050A GB 195050 A GB195050 A GB 195050A GB 5356/23 A GB5356/23 A GB 5356/23A GB 535623 A GB535623 A GB 535623A GB 195050 A GB195050 A GB 195050A
- Authority
- GB
- United Kingdom
- Prior art keywords
- hardened
- hardening
- blade
- blades
- places
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
195.050. Akt.-Ges. Brown, Boveri, et Cie. March 18, 1922, [Convention date]. Case-hardening. - Blades for steam turbines are hardened only in those parts which are most exposed to erosion, more particularly the upper part of the leading edge of the blade as indicated by hatchings, Fig. 2. The whole of the edges may be hardened as indicated in Figs. 3 and 4, the head of the blade being left soft to facilitate riveting the binding ring a. One method of making the blades consists in employing a material which of itself cannot be hardened. and coating this material at the places where it is not to be hardened with, for example, an electrolytic deposit which does not allow any carbon to penetrate, and then, by a casehardening operation, enriching the unprotected places with carbon, and then hardening such places by subsequent quenching. To prevent distortion, the blade, before quenching, may be clamped in a rigid mould, or be bent in the opposite direction to compensate for the distortion due to the hardening. Those parts of the hardened blade which are to remain soft may be softened again by tempering after the hardening.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE195050X | 1922-03-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB195050A true GB195050A (en) | 1923-07-19 |
Family
ID=5747534
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5356/23A Expired GB195050A (en) | 1922-03-18 | 1923-02-23 | Improvements in steam turbine blades, and in the method of manufacturing such blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB195050A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2783967A (en) * | 1952-01-03 | 1957-03-05 | Maschf Augsburg Nuernberg Ag | Ceramic machine parts |
US3275295A (en) * | 1964-06-12 | 1966-09-27 | English Electric Co Ltd | Turbine blade with tapered one-piece erosion shield |
US3834833A (en) * | 1972-02-18 | 1974-09-10 | Bbc Brown Boveri & Cie | Blade construction for axial-flow turbo-machines and method of protecting turbo-machine blades against stress corrosion cracking |
EP0379922A1 (en) * | 1989-01-24 | 1990-08-01 | Refurbished Turbine Components Limited | Turbine blade repair |
US5531570A (en) * | 1995-03-06 | 1996-07-02 | General Electric Company | Distortion control for laser shock peened gas turbine engine compressor blade edges |
US5785498A (en) * | 1994-09-30 | 1998-07-28 | General Electric Company | Composite fan blade trailing edge reinforcement |
EP1382799A2 (en) * | 2002-07-20 | 2004-01-21 | Rolls Royce Plc | Gas turbine engine casing and rotor blade arrangement |
-
1923
- 1923-02-23 GB GB5356/23A patent/GB195050A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2783967A (en) * | 1952-01-03 | 1957-03-05 | Maschf Augsburg Nuernberg Ag | Ceramic machine parts |
US3275295A (en) * | 1964-06-12 | 1966-09-27 | English Electric Co Ltd | Turbine blade with tapered one-piece erosion shield |
US3834833A (en) * | 1972-02-18 | 1974-09-10 | Bbc Brown Boveri & Cie | Blade construction for axial-flow turbo-machines and method of protecting turbo-machine blades against stress corrosion cracking |
EP0379922A1 (en) * | 1989-01-24 | 1990-08-01 | Refurbished Turbine Components Limited | Turbine blade repair |
US5785498A (en) * | 1994-09-30 | 1998-07-28 | General Electric Company | Composite fan blade trailing edge reinforcement |
US5531570A (en) * | 1995-03-06 | 1996-07-02 | General Electric Company | Distortion control for laser shock peened gas turbine engine compressor blade edges |
EP1382799A2 (en) * | 2002-07-20 | 2004-01-21 | Rolls Royce Plc | Gas turbine engine casing and rotor blade arrangement |
EP1382799A3 (en) * | 2002-07-20 | 2005-09-07 | Rolls Royce Plc | Gas turbine engine casing and rotor blade arrangement |
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