GB190811885A - Improvements in and relating to Means for Balancing the End Pressure in Turbines. - Google Patents
Improvements in and relating to Means for Balancing the End Pressure in Turbines.Info
- Publication number
- GB190811885A GB190811885A GB190811885DA GB190811885A GB 190811885 A GB190811885 A GB 190811885A GB 190811885D A GB190811885D A GB 190811885DA GB 190811885 A GB190811885 A GB 190811885A
- Authority
- GB
- United Kingdom
- Prior art keywords
- packings
- turbine
- pressure
- turbines
- space
- 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
11,885. Roth, C. June 11, 1907, [date applied for under Section 91 of Patents &c. Act, 1907]. [Patent of Addition to No. 6738, A.D 1908.] Elastic-fluid turbines.-End pressure in turbines is balanced by means of a number of dummy pistons, and suitable packings are so arranged that the dummy pistons and the packings are subjected to only a part of the total pressure. The packings may be placed at the high or low pressure end of the turbine or at both ends. In the form shown in Fig. 1 the intermediate space s is connected by a pipe to the space between the two packings o', o<2>, and the interior of the turbine communicates with the condenser space k. The annular surface between the diameter d' of the rotor and the packing o<1> forms one dummy piston, and the surface between the packings o<1>, o<2> forms a second dummy piston. In other forms of turbine described the interior of the drum is connected to the condenser or to the space between the first stages of the turbine. Reversing turbines are also described with one packing at each high-pressure end, Fig. 6, and also with packings for each turbine similar to that shown in Fig. 1. In the turbine, Fig. 6. the interior of the drum is connected to exhaust pressure, and packings at the high-pressure ends are used. On the nozzle ring between the two velocity stages c, c<2> a packing e is used comprising a number of ledges 9, 9<1>, 9<2>, Figs. 10 and 11, coacting with ledges 8, 8<1>, 8<2> on the rotor. The ledges may be caulked in or otherwise fixed to their supporting- members, or may be formed in one therewith. Similar packings may be used for the blades. In one form of turbine shown an overload valve is used to pass steam to the second stage directly from the steam-pipe.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE190806738X | 1907-04-02 | ||
DE190811885X | 1907-06-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB190811885A true GB190811885A (en) | 1908-12-31 |
Family
ID=32232106
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190811885D Expired GB190811885A (en) | 1907-04-02 | 1908-06-01 | Improvements in and relating to Means for Balancing the End Pressure in Turbines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB190811885A (en) |
-
1908
- 1908-06-01 GB GB190811885D patent/GB190811885A/en not_active Expired
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