Curioustab
Aptitude
General Knowledge
Verbal Reasoning
Computer Science
Interview
Aptitude
General Knowledge
Verbal Reasoning
Computer Science
Interview
Steam Nozzles and Turbines Questions
The pressure velocity compounded impulse turbine allows a bigger pressure drop and hence __________ number of stages are required.
In velocity compounding of an impulse turbine, the expansion of steam takes place in a nozzle or a set of nozzles from the boiler pressure to condenser pressure.
If the critical pressure ratio for steam is 0.546, then the steam is initially
In a Parson's turbine stage, blade velocity is 320 m/s at the mean radius and rotor blade exit angle is 30°. For minimum kinetic energy of the steam leaving the stage, the steam velocity at the exit of the rotor will be
In an impulse turbine, steam expands
A nozzle is said to be a convergent-divergent nozzle, when the cross-section of a nozzle first decreases from its entrance to throat and then increases from its throat to exit.
In an ideal impulse turbine, the
The effect of bleeding is that
A single stage turbine is not used because it requires large reduction gearing due to very high rotational speed.
Which of the following statement is wrong?
During flow through a nozzle, no heat is supplied or rejected by the steam.
Which of the following statement is correct?
Steam turbines may be classified according to
In a nozzle, the effect of supersaturation is to increase the dryness fraction of steam.
In a nozzle, the effect of supersaturation is to
For a Parson's reaction turbine, if α1 and α2 are fixed blade angles at inlet and exit respectively and β1 and β2 are the moving blade angles at entrance and exit respectively, then
When the cross-section of a nozzle __________ continuously from entrance to exit, it is called a convergent nozzle.
The efficiency of an impulse turbine is maximum when (where Vb = Blade speed, V = Absolute velocity of steam entering the blade, and α = Nozzle angle)
The expansion of steam in a nozzle follows
In a 50% reaction turbine stage, tangential component of absolute velocity at rotor inlet is 537 m/s and the blade velocity is 454 m/s. The power output in kW of steam will be
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