Rotary machine
A technology for rotating machinery and rotating shafts, applied in mechanical equipment, engine functions, engine components, etc., can solve the problems of increased material and manufacturing costs, increased size of rotating machinery, increased housing size, etc., to achieve enhanced reliability and performance, maintaining The effect of enhanced precision and enhanced reliability
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no. 1 approach
[0037] will refer to Figure 1-5 A casing structure having a gas turbine according to an embodiment of the present invention and a gas turbine having such a casing structure are described.
[0038] figure 1 is a schematic diagram for describing the overall structure of the gas turbine according to the first embodiment of the present invention.
[0039] Such as figure 1 As shown, a gas turbine (rotary machine) 100 includes a housing 101 constituting the outer shape of the gas turbine 100, a blade ring 3 holding the turbine stator blades 10 on its inner circumference, a rotating shaft 4 embedded with the turbine rotor blades 11, and a turbine stator. The first stage of the blade 10 provides an inlet scroll portion 5 for the working fluid, a discharge scroll portion 6 into which the working fluid discharged from the last stage of the turbine rotor blade 11 flows.
[0040] In the gas turbine 100, the working fluid is accelerated by the turbine stator blades 10, the turbine roto...
no. 2 approach
[0074] Figure 4 is a schematic diagram for describing the overall structure of a gas turbine according to a second embodiment of the present invention. The main structure of the gas turbine of this embodiment is the same as that of the first embodiment, and the holding structure of the third connecting flange is different from that of the first embodiment. In this example, reference will be made to Figure 4 Only the holding structure of the third connection flange will be described, and descriptions of other constituent elements will not be repeated. The same constituent elements as those of the first embodiment are denoted by the same reference numerals, and description thereof will not be repeated.
[0075] In the second embodiment, as Figure 4 As shown, the outer peripheral surface of flange 3A sandwiched between flanges 1A and 1B of casings 1 and 2 obtained by dividing casing 101 of gas turbine 300 into two is bonded between flanges 1A and 1B.
[0076] In the first ...
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