Steam Turbine, and Steam Turbine Stationary Blade
a steam turbine and stationary blade technology, applied in the field of steam turbines, can solve the problems of reducing the reliability the inability to always set the erosion shield, and the erosive action of the blade surface, so as to reduce the erosive action and improve the reliability
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embodiment 1
[0036]A first embodiment according to the present invention will be described.
[0037]FIGS. 3 to 5 are explanatory diagrams showing the structure where the preset invention is applied to the stationary blade 1 in FIG. 1. FIG. 3 is a schematic perspective diagram of the stationary blade 1 according to the present embodiment, FIG. 4, a cross-sectional diagram in a position indicated with an alternate long and two short dashes line in FIG. 3, and FIG. 5, an enlarged diagram of a blade tail part in FIG. 4.
[0038]As shown in FIG. 3, the stationary blade 1 of the present embodiment is formed by joining a main body 5 and a blade tail part 8 formed as a separate body of the main body 5 along a welding line 9. As shown in FIG. 4, the main body 5 is formed by plastically deforming a metal plate by pressing or the like, and has a hollow blade shape structure having a hollow part 26 inside. On the other hand, the tail part 8 has a suction side plate 20 which is a metal plate forming a suction side...
embodiment 2
[0053]Next, a second embodiment of the present invention will be described using FIG. 7. In the present embodiment, the slit is not formed in the entire region in the stationary blade height direction, but limitedly in a region opposite to the tip part of the moving blade 2 shown in FIG. 1.
[0054]The liquid film is eliminated with the slit 24 and the second slit 23, however, the steam is also sucked at the same time of the elimination of the liquid film. The increment of the steam removal directly influences the degradation of the performance of the steam turbine. Further, the erosion amount by the liquid droplets flying from the stationary blade is increased in accordance with the increment of the circumferential velocity of the moving blade. Accordingly, the blade structure in the 70% or greater region in the blade height direction is formed with the joint body between the main body 5 and the blade tail part 8 shown in the embodiment 1.
[0055]In the present embodiment, it is possibl...
embodiment 3
[0057]Next, a third embodiment of the present invention is shown in FIG. 8 and FIG. 9. FIG. 8 shows a cross-section of the stationary blade according to the third embodiment, and FIG. 9 is an enlarged diagram of the blade tail part of the stationary blade shown in FIG. 8.
[0058]In the present embodiment, the blade tail part 8 is not formed completely independently of the main body 5, but the member forming the blade surface of the main body 5 is extended and applied to the suction side plate 20 of the blade tail part 8. That is, on the suction side of airfoil, the main body 5 and the blade tail part 8 are formed with one metal plate. On the other hand, on the pressure side of airfoil, as in the case of the embodiment 1, the metal plates forming the main body 5 and the blade tail part 8 are separate bodies. The pressure side plate 21 is overlaid on the step part 27 of the suction side plate 20 integrally formed with the main body 5 with a gap therebetween, and its one end is welded an...
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