In Parsons’ reaction turbine, the velocity diagram triangles at the inlet and outlet are
congruent
Parsons' reaction turbine is a significant design in steam turbine technology, primarily known for its 50% degree of reaction. This means the process of energy conversion is equally distributed between the stationary blades (nozzles) and the moving blades (rotor). A key characteristic resulting from this design principle is observed in the velocity diagrams at the inlet and outlet of the moving blades.
Velocity diagrams are essential tools in turbomachinery analysis. They graphically represent the relationship between three key velocities:
These velocities form vector triangles at the inlet and outlet points of the moving blades, providing insights into the energy transfer and flow dynamics.
In a Parsons' reaction turbine, the specific condition of a 50% reaction implies a balance in how the steam expands and accelerates through the stationary and moving blade rows. This balance leads to a specific relationship between the inlet and outlet velocity triangles for the moving blades.
For a 50% reaction turbine, the following conditions are met:
Because the corresponding sides and angles are equal ($W_1 = W_2$, $V_1 = V_2$, and $U$ is common), the velocity triangles formed at the inlet and outlet of the moving blades are identical. This means the triangles are congruent.
The defining characteristic of the velocity diagram triangles at the inlet and outlet of the moving blades in a Parsons' reaction turbine is their congruence. This congruence is a direct consequence of the turbine's 50% reaction design, ensuring an even distribution of energy conversion across both stator and rotor stages.
A draft tube is used with _____.
Reaction turbines are used for _____
When a hydraulic turbine is operated, it is found that it has a high design efficiency and this efficiency remains constant over a wide range of regulations from the design condition. What is the type of this turbine?
For a non-dimensional specific speed value of 1, for maximum efficiency, which of the following turbines is preferred?