GB452027A - Improvements in and relating to turbine blades - Google Patents
Improvements in and relating to turbine bladesInfo
- Publication number
- GB452027A GB452027A GB4887/35A GB488735A GB452027A GB 452027 A GB452027 A GB 452027A GB 4887/35 A GB4887/35 A GB 4887/35A GB 488735 A GB488735 A GB 488735A GB 452027 A GB452027 A GB 452027A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sections
- faces
- blades
- molten metal
- packing
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
452,027. Making turbines. PARSONS MARINE STEAM TURBINE CO., Ltd., and BROWN, D S., Turbina Works, Wallsend-on-Tyne. Feb. 15, 1935, No. 4887. [Classes 83 (ii) and 83 (iv)] [See also Group XXVI] Soldering.-A number of turbine blades provided with intermediate packing sections, which are to be secured together by being dipped in molten metal, have spaces arranged between the faces of the blades and sections, to permit easy access of a suitable flux, such as a solution of borax, and afterwards the molten metal. Parallel ridges d may be formed on the faces of the sections b, or three or more circular or other-shaped projections arranged triangularly on the section faces. Alternatively the blade edges may be corrugated. The blades and packing may be temporarily held in place by a wire threaded through the roots, by tack welding, or by a shroud. Specification 16284/99, [Class 83], is referred to.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL40782D NL40782C (en) | 1935-02-15 | ||
GB4887/35A GB452027A (en) | 1935-02-15 | 1935-02-15 | Improvements in and relating to turbine blades |
US62741A US2090468A (en) | 1935-02-15 | 1936-02-07 | Turbine blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4887/35A GB452027A (en) | 1935-02-15 | 1935-02-15 | Improvements in and relating to turbine blades |
Publications (1)
Publication Number | Publication Date |
---|---|
GB452027A true GB452027A (en) | 1936-08-17 |
Family
ID=9785716
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4887/35A Expired GB452027A (en) | 1935-02-15 | 1935-02-15 | Improvements in and relating to turbine blades |
Country Status (3)
Country | Link |
---|---|
US (1) | US2090468A (en) |
GB (1) | GB452027A (en) |
NL (1) | NL40782C (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2654143A (en) * | 1949-08-24 | 1953-10-06 | Allis Chalmers Mfg Co | Method of making welded blade structures |
US2808228A (en) * | 1950-08-01 | 1957-10-01 | Rolls Royce | Turbo-machines |
US2807435A (en) * | 1951-06-12 | 1957-09-24 | Fairchild Engine & Airplane | Turbine stator blade |
US2894318A (en) * | 1952-10-08 | 1959-07-14 | Gen Electric | Turbomachine bucket-wheel fabricated by casting |
-
0
- NL NL40782D patent/NL40782C/xx active
-
1935
- 1935-02-15 GB GB4887/35A patent/GB452027A/en not_active Expired
-
1936
- 1936-02-07 US US62741A patent/US2090468A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
NL40782C (en) | |
US2090468A (en) | 1937-08-17 |
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