Q.1.
Calculate the mean blade velocity of a Parson’s reaction turbine, if the steam leaves the nozzle with an absolute velocity ofm/s. Take the nozzle angle asand the turbine works at maximum efficiency.
Q.2.
The nozzle angle of a Parson’s reaction turbine is 25°. Determine the maximum possible efficiency for the turbine.
Q.3.
The efficiency of steam turbine is greater than that of gas turbines.
Q.4.
The following data refer to a particular stage of a Parson’s reaction turbine:
Q.5.
In a reaction turbine, the fixed blades and moving blades are of the same shape but reversed in direction. The angle of the discharging tip is 20°. The mean blade velocity ism/s. The axial velocity of flow of steam is half of the mean blade velocity. Determine the inlet angles of blades.
Q.6.
Areaction turbine, having symmetrical velocity triangles, runs atr.p.m. The exit angles of the blades are 20°. The speed ratio is 0.8 and the diameter of the rotor blades is 1 meter. Determine the power developed if the mass flow rate of steam is 0.kg per second.
Q.7.
In a steam turbine the turbine blade’s tip experiences more erosion than any other part.
Q.8.
Which of the following is the correct definition for ‘Adiabatic Power’?
Q.9.
Which of the following is the correct definition of ‘Shaft Power’?
Q.10.
Which of the following statements regarding a Reaction turbine is FLASE?