This invention relates to a water turbine of the reaction type, such as a Francis or Kaplan turbine, comprising a rotor and a surrounding housing, with seal means between the rotor and the housing.
In this type of turbines there is a problem in that a large part the losses is connected with seal leakage. Today simple labyrinth seals are often used, but they require large clearances and so have large losses. In this connection the dimensions of the structures involved, are to be considered; and traditional axle seals are not of interest here.
U.S. Pat. No. 4,464,580 (Miller) is an example of a conventional hydro turbine provided with seals at locations corresponding to what is of interest to the present invention, i.e. at appreciable radial distances from the axis of the rotor. These known seals are lip seals.
U.S. Pat. No. 4,293,777 (Gamell) is directed to a very special type of turbine (“drag turbine”) provided with brush seals, these being a kind of axle seals subjected to low head pressures.
U.S. Pat. No. 6,406,027 (General Electric Company) describes brush seals in rotary machines, with an emphasis on steam and gas turbines, where the particular design and structure of the seals are at focus. Mainly axle seals are considered.
U.S. Pat. No. 6,913,265 (Datta) also relates to the design of a brush seal as such.
From the above it is apparent that brush seals are known in particular for use in gas turbines and the like.
On this background it is an important object of the present invention to provide a water turbine seal system that makes possible much smaller clearances than current labyrinth and other conventional seal designs for the purpose discussed above, so as to obtain an efficiency improvement in high head Francis turbines, inter alia.
This is obtained, according to the invention by providing in a water turbine as stated in the first paragraph above, sealing means comprising brush seals located at a radial distance from the rotor axis being a major proportion of the maximum radial dimension of the rotor. Thus, surprisingly brush seals have been found useful in clearances between the rotor and the housing in the types of water turbines being of interest here.
Advantages obtained with the solution according to the invention, are:
In the following description an example of a turbine design based on this invention will be explained more in detail, with reference to the drawing, where
a is an enlarged detail in the structure of
As conventional the illustrated turbine comprises a rotor 2 having an axis of rotation 1, this axis being vertical in this example. Housing structure 5 surrounds the rotor and comprises a guide vane duct 5 for directing water towards the rotor 2. Leakage of this water in clearances between housing parts and closely adjacent portions of the rotor, should be prevented as much as possible. For this purpose there is provided for sealing as indicated at 10 and 20.
The seal 10 is shown more in detail in
The location of the brush seals 10 and 20 should be noted, since according to the invention and in particular with turbines having a vertical axis of rotation, both seals 10 and 20 have positions approximately at the same radial distance from the axis 1. In this respect, however, modifications as to the radial position of upper (10) and lower (20) seals may vary according to the turbine design concerned. Although in many designs seal positions at approximately the same and/or maximum radial distance from the axis, would be preferred, other options are possible. What is important is that the radial distances of the seals from the axis, are a major proportion of the maximum radial dimension of the rotor. This shows that what is here of interest, has nothing to do with traditional axle sealing.
Number | Date | Country | Kind |
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20063088 | Jul 2006 | NO | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/NO2007/000230 | 6/25/2007 | WO | 00 | 9/22/2009 |