| 摘要 |
<p>A reaction turbine, according to the present invention, comprises first and second rotor plates, which are coupled together to form an integrated rotor, and an inner flow path comprising a combination of first and second flow paths, which are formed on the surfaces of the first and second rotor plates that face each other, respectively, thereby enabling easier manufacturing into a form desired by a designer by eliminating the limitation of a cross-sectional shape of the inner flow path. In addition, a cross section of each of the first and second flow paths can be formed into a semicircular shape thus yielding a circular shape for the inner flow path, which is formed by combining the first and second flow paths, thereby effectively enhancing the performance of a turbine by minimizing pressure loss of an operation fluid that passes through the inner flow path.</p> |
