GB683848A - Improvements in and relating to welding - Google Patents
Improvements in and relating to weldingInfo
- Publication number
- GB683848A GB683848A GB22085/50A GB2208550A GB683848A GB 683848 A GB683848 A GB 683848A GB 22085/50 A GB22085/50 A GB 22085/50A GB 2208550 A GB2208550 A GB 2208550A GB 683848 A GB683848 A GB 683848A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sept
- roots
- pieces
- sections
- weld metal
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
- F01D5/063—Welded rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K33/00—Specially-profiled edge portions of workpieces for making soldering or welding connections; Filling the seams formed thereby
- B23K33/004—Filling of continuous seams
- B23K33/008—Filling of continuous seams for automotive applications
Abstract
683,848. Welding by fusion. BRITISH THOMSON-HOUSTON CO., Ltd. Sept. 7, 1950 [Sept. 23, 1949], No. 22085/50. Class 83 (iv). An overlapping welded joint comprises proximate pieces of metal having root sections extending therefrom, the inner surfaces of which are overlapped to form a single interstice therebetween extending in a single direction only which is substantially parallel to stresses set up by centrifugal force to which the pieces are to be subjected, grooved portions being machined from opposite surfaces of each piece, separated by the roots sections, to form substantially symmetrical spaces for the deposit of weld metal. In one embodiment, a rotor rim 10 of a gas turbine wheel is welded to a hub 9 arranged so that roots 12, 13 overlap and form grooves 14, 15 in which weld metal is deposited from an arc stream. There is no necessity to chip out the root sections.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US683848XA | 1949-09-23 | 1949-09-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB683848A true GB683848A (en) | 1952-12-03 |
Family
ID=22082218
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB22085/50A Expired GB683848A (en) | 1949-09-23 | 1950-09-07 | Improvements in and relating to welding |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB683848A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105386794A (en) * | 2015-12-10 | 2016-03-09 | 西安航天动力研究所 | Turbine disc rigidity self-reinforcement turbine structure |
-
1950
- 1950-09-07 GB GB22085/50A patent/GB683848A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105386794A (en) * | 2015-12-10 | 2016-03-09 | 西安航天动力研究所 | Turbine disc rigidity self-reinforcement turbine structure |
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