GB190406380A - Improvements in Fluid Pressure Turbines. - Google Patents
Improvements in Fluid Pressure Turbines.Info
- Publication number
- GB190406380A GB190406380A GB190406380DA GB190406380A GB 190406380 A GB190406380 A GB 190406380A GB 190406380D A GB190406380D A GB 190406380DA GB 190406380 A GB190406380 A GB 190406380A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- vanes
- exploded
- guide
- controlling
- 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
- Control Of Turbines (AREA)
Abstract
6380. Smith, H., and Lewis, E. W. March 16. Gas turbines.-A turbine having a number of rotary open-ended explosion chambers is shown in Figs. 1 and 2. The turbine wheel has a number of curved explosion chambers A open at their outer ends and closed at their inner ends by a conical hub C having admission valves A<2> controlling the air supply from a fan J, and also controlling the supply of explosive fluid admitted through passages C<5> in the shaft and hub. The wheel is surrounded by an incomplete ring of guide-vanes F, an imperforate partition F<1> allowing the explosive mixture to be compressed before being exploded. The valves are actuated by levers G pivoted at one end, and having rollers G<2> at the other end arranged progressively so that one or more can be acted on by a cam H adjusted by toothed gearing H<2>. The mixture is exploded by sparking-plugs K, and the explosion is timed to take place as each chamber approaches the guide-vanes. Part of the exhaust escapes into a passage L<2> through a nozzle L, and the ejector action thus produced draws the remainder of the exhaust through a pipe L<5> opening into the opposite side of the turbine casing.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB190406380T | 1904-03-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB190406380A true GB190406380A (en) | 1905-01-26 |
Family
ID=32624719
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190406380D Expired GB190406380A (en) | 1904-03-16 | 1904-03-16 | Improvements in Fluid Pressure Turbines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB190406380A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2633922A (en) * | 1946-04-09 | 1953-04-07 | Helge S G Svenson | Jet-propulsion mechanism |
-
1904
- 1904-03-16 GB GB190406380D patent/GB190406380A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2633922A (en) * | 1946-04-09 | 1953-04-07 | Helge S G Svenson | Jet-propulsion mechanism |
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