GB190706640A - Improvements in the Construction of Guide-blades and Vanes for Turbine Motors. - Google Patents
Improvements in the Construction of Guide-blades and Vanes for Turbine Motors.Info
- Publication number
- GB190706640A GB190706640A GB190706640DA GB190706640A GB 190706640 A GB190706640 A GB 190706640A GB 190706640D A GB190706640D A GB 190706640DA GB 190706640 A GB190706640 A GB 190706640A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- foot
- plate
- plates
- morcom
- 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
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
6640. Belliss & Morcom, and Morcom, R. K. March 19. Elastic-fluid turbines.-Relates to making and fixing blades for turbine rotors and stators. Thin metal stampings are bent so as to form the front and back plates or surfaces a, b, Figs. 1, 2 and 9, of two'adjacent blades connected by a foot c, the plates being also united by one or more thin distance-pieces g; the back plate may have a strengthening-rib b<2>. The blades are formed by assembling a number of these blade elements, the feet being secured in undercut grooves by bifurcated retaining-blocks e and a stringer f, which spreads the fangs and flattens the arched foot. The widths of the front and back plates may vary so that the edge of the blade, which may be sharpened, may have one or two thicknesses of metal. Composite blade elements are stamped out of a composite metal sheet, for example from a steel strip A, Fig. 7, and a copper strip B welded or brazed together so that the stamping has an erosionresisting front plate a and a bendable back-plate b and foot c.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB190706640T | 1907-03-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB190706640A true GB190706640A (en) | 1908-03-19 |
Family
ID=32548148
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190706640D Expired GB190706640A (en) | 1907-03-19 | 1907-03-19 | Improvements in the Construction of Guide-blades and Vanes for Turbine Motors. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB190706640A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2421360A (en) * | 1941-04-05 | 1947-05-27 | Borg Warner | Fluid coupling |
US2656146A (en) * | 1948-04-08 | 1953-10-20 | Curtiss Wright Corp | Turbine blade construction |
US2658718A (en) * | 1944-12-22 | 1953-11-10 | Power Jets Res & Dev Ltd | Manufacture and attachment of turbine and like blading |
-
1907
- 1907-03-19 GB GB190706640D patent/GB190706640A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2421360A (en) * | 1941-04-05 | 1947-05-27 | Borg Warner | Fluid coupling |
US2658718A (en) * | 1944-12-22 | 1953-11-10 | Power Jets Res & Dev Ltd | Manufacture and attachment of turbine and like blading |
US2656146A (en) * | 1948-04-08 | 1953-10-20 | Curtiss Wright Corp | Turbine blade construction |
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