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Mechanical Engineering
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Steam Nozzles and Turbines
Comments
Question
The impulse turbine rotor efficiency will have a maximum value of 0.5 cos
2
?, where ? is the nozzle exit flow angle, if the
Options
A. blades are equiangular
B. blade velocity coefficient is unity
C. blades are equiangular and frictionless
D. blade solidity is 0.65
Correct Answer
blades are equiangular and frictionless
Steam Nozzles and Turbines problems
Search Results
1. A steam nozzle converts
Options
A. heat energy of steam into kinetic energy
B. kinetic energy into heat energy of steam
C. heat energy of steam into potential energy
D. potential energy into heat energy of steam
Show Answer
Scratch Pad
Discuss
Correct Answer: heat energy of steam into kinetic energy
2. When the cross-section of a nozzle increases continuously from entrance to exit, it is called a
Options
A. divergent nozzle
B. convergent nozzle
C. convergent-divergent nozzle
D. none of these
Show Answer
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Discuss
Correct Answer: divergent nozzle
3. The purpose of governing in steam turbines is to
Options
A. maintain the speed of the turbine
B. reduce the effective heat drop
C. reheat the steam and improve its quality
D. completely balance against end thrust
Show Answer
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Discuss
Correct Answer: maintain the speed of the turbine
4. Rateau turbine is
Options
A. simple reaction turbine
B. velocity compounded turbine
C. pressure compounded turbine
D. pressure-velocity compounded turbine
Show Answer
Scratch Pad
Discuss
Correct Answer: pressure compounded turbine
5. In a velocity compounded impulse turbine, when steam flows through the second row of moving blades,
Options
A. velocity increases
B. velocity decreases
C. velocity remains constant
D. pressure remains constant
Show Answer
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Discuss
Correct Answer: velocity decreases
6. The density of supersaturated steam is about __________ that of the ordinary saturated vapour at the corresponding pressure.
Options
A. same as
B. 2 times
C. 4 times
D. 8 times
Show Answer
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Discuss
Correct Answer: 8 times
7. The flow of steam is super-sonic
Options
A. at the entrance to the nozzle
B. at the throat of the nozzle
C. in the convergent portion of the nozzle
D. in the divergent portion of the nozzle
Show Answer
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Discuss
Correct Answer: in the divergent portion of the nozzle
8. Curtis turbine is a
Options
A. simple reaction turbine
B. velocity compounded turbine
C. pressure compounded turbine
D. pressure-velocity compounded turbine
Show Answer
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Discuss
Correct Answer: pressure-velocity compounded turbine
9. The diagram efficiency is the ratio of
Options
A. workdone on the blades to the energy supplied to the blades
B. workdone on the blades per kg of steam to the total energy supplied per stage per kg of steam
C. energy supplied to the blades per kg of steam to the total energy supplied per stage per kg of steam
D. none of the above
Show Answer
Scratch Pad
Discuss
Correct Answer: workdone on the blades to the energy supplied to the blades
10. The velocity of steam, in reaction turbines, is increased in the fixed blades as well as in moving blades.
Options
A. True
B. False
Show Answer
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Discuss
Correct Answer: True
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