GB636084A - Improvements in and relating to runners of hydraulic turbines - Google Patents
Improvements in and relating to runners of hydraulic turbinesInfo
- Publication number
- GB636084A GB636084A GB31181/47A GB3118147A GB636084A GB 636084 A GB636084 A GB 636084A GB 31181/47 A GB31181/47 A GB 31181/47A GB 3118147 A GB3118147 A GB 3118147A GB 636084 A GB636084 A GB 636084A
- Authority
- GB
- United Kingdom
- Prior art keywords
- deposit
- blade
- grinding
- blades
- composite
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
- B23P6/005—Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
- F03B3/12—Blades; Blade-carrying rotors
- F03B3/121—Blades, their form or construction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/20—Hydro energy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Hydraulic Turbines (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
Abstract
636,084. Making turbines and composite turbine blades. ENGLISH ELECTRIC CO., Ltd., and DERIAZ, P. Nov. 25, 1947, No. 31181. [Class 83 (ii)] [Also in Group XXVI] Blades for hydraulic turbine runners are made by cutting a flat plate of mild steel to the shape required for the blade, applying a deposit of stainless steel by electric welding so as to protect it against erosion, machining and/or grinding the composite plate to a smooth surface finish and accurate thickness and then bending the composite flat plate to the required shape of the blade. The runner may be made by assembling the completed blades in required position and integrating them by casting the hubs and shroud rings on their edges or by welding thereto separately made hubs and shroud rings. The blade may be coated only at the mainly endangered region as at 7, the flat plate being previously recessed by milling or grinding to receive the deposited metal, and the machining or grinding limited to the region of the deposit to make it flush with the rest of the plate. The flat plates may be given a streamlined profile after applying the deposit by taking material mainly off the opposite surface.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB31181/47A GB636084A (en) | 1947-11-25 | 1947-11-25 | Improvements in and relating to runners of hydraulic turbines |
ES0186051A ES186051A1 (en) | 1947-11-25 | 1948-11-24 | A PROCEDURE OF PRODUCING BLADES FOR HYDRAULIC TURBINE ROTORS |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB31181/47A GB636084A (en) | 1947-11-25 | 1947-11-25 | Improvements in and relating to runners of hydraulic turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB636084A true GB636084A (en) | 1950-04-19 |
Family
ID=10319213
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB31181/47A Expired GB636084A (en) | 1947-11-25 | 1947-11-25 | Improvements in and relating to runners of hydraulic turbines |
Country Status (2)
Country | Link |
---|---|
ES (1) | ES186051A1 (en) |
GB (1) | GB636084A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4776765A (en) * | 1985-07-29 | 1988-10-11 | General Electric Company | Means and method for reducing solid particle erosion in turbines |
FR2916667A1 (en) * | 2007-06-01 | 2008-12-05 | Alstom Power Hydraulique Sa | Vane or blade manufacturing method for reaction turbine, involves assembling two sheets of different thicknesses to form assembly, shaping assembly of two sheets, and removing material from assembly of sheets by machining |
CN1912380B (en) * | 2005-07-14 | 2013-01-02 | 通用电器(加拿大)公司 | Split francis turbine runner |
CN103506801A (en) * | 2013-09-24 | 2014-01-15 | 四川蜀港水电工程技术有限责任公司 | Process for cavitation repair welding of through-flow turbine set runner chamber |
CN106392459A (en) * | 2016-10-18 | 2017-02-15 | 西安航空制动科技有限公司 | Method for correcting deformation of aluminum alloy half snap ring through prestress shot peening |
-
1947
- 1947-11-25 GB GB31181/47A patent/GB636084A/en not_active Expired
-
1948
- 1948-11-24 ES ES0186051A patent/ES186051A1/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4776765A (en) * | 1985-07-29 | 1988-10-11 | General Electric Company | Means and method for reducing solid particle erosion in turbines |
CN1912380B (en) * | 2005-07-14 | 2013-01-02 | 通用电器(加拿大)公司 | Split francis turbine runner |
FR2916667A1 (en) * | 2007-06-01 | 2008-12-05 | Alstom Power Hydraulique Sa | Vane or blade manufacturing method for reaction turbine, involves assembling two sheets of different thicknesses to form assembly, shaping assembly of two sheets, and removing material from assembly of sheets by machining |
CN103506801A (en) * | 2013-09-24 | 2014-01-15 | 四川蜀港水电工程技术有限责任公司 | Process for cavitation repair welding of through-flow turbine set runner chamber |
CN106392459A (en) * | 2016-10-18 | 2017-02-15 | 西安航空制动科技有限公司 | Method for correcting deformation of aluminum alloy half snap ring through prestress shot peening |
Also Published As
Publication number | Publication date |
---|---|
ES186051A1 (en) | 1949-02-16 |
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