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Mechanical Engineering : Hydraulic Machines - Quiz(MCQ)
A)
Mechanical Energy
B)
Elastic Energy
C)
Nuclear Energy
D)
Electrical Energy

Correct Answer :   Mechanical Energy


Explanation : Hydraulic machines firstly convert the energy possessed by water into mechanical energy. Later it can be transformed into electrical energy.

A)
Braggs law
B)
Faraday law
C)
Charles law
D)
Newton’s second law

Correct Answer :   Newton’s second law


Explanation : A Hydraulic Machine uses the principle of momentum which states that a force is generated which is utilized in a turbine.

A)
Switch off the turbine
B)
To regenerate the power
C)
Alter the direction of water
D)
To regulate the wind speed

Correct Answer :   Alter the direction of water


Explanation : Turbines use blades and buckets to alter the direction of water. It is used to change the momentum of water. As momentum changes, force is produced to rotate the shaft of a hydraulic machine.

A)
low velocity
B)
high velocity
C)
low pressure
D)
high pressure

Correct Answer :   low pressure

A)
N/H
B)
N/√H
C)
N/H²
D)
N/H³

Correct Answer :   N/√H

A)
impeller
B)
casing
C)
suction pipe
D)
delivery pipe

Correct Answer :   delivery pipe

A)
True
B)
False
C)
Can Not Say
D)
None of the above

Correct Answer :   False

A)
directly
B)
inversely
C)
Can Not Say
D)
None of the above

Correct Answer :   directly

9 .
The force exerted (in newton) by a jetof water impinging normally on a fixed plate is (where w = Specific weight of water in N/m³, a = Cross-sectional area of jet in m², and V = Velocity of jet in m/s)
A)
waV/g
B)
waV/2g
C)
waV²/g
D)
waV²/2g

Correct Answer :   waV²/g

10 .
The unit power developed by a turbine is (where P = Power developed by the turbine under a head of water (H))
A)
P/√H
B)
P/H
C)
P/H2
D)
P/H3/2

Correct Answer :   P/H3/2

A)
directly proportional to N
B)
inversely proportional to N
C)
directly proportional to N²
D)
inversely proportional to N²

Correct Answer :   directly proportional to N²

12 .
A Pelton wheel develops 1750 kW under a head of 100 metres while running at 200 r.p.m. and discharging 2500 litres of water per second. The unit discharge of wheel is
A)
0.25 m³/s
B)
0.5 m³/s
C)
1.5 m³/s
D)
2.5 m³/s

Correct Answer :   0.25 m³/s

13 .
The power developed by a turbine is (where H = Head of water under which the turbine is working)
A)
directly proportional to H1/2
B)
directly proportional to H3/2
C)
inversely proportional to H1/2
D)
inversely proportional to H3/2

Correct Answer :   directly proportional to H3/2

A)
diameter
B)
cube of diameter
C)
fourth power of diameter
D)
square of diameter

Correct Answer :   fourth power of diameter

A)
ratio of the Work done on the wheel to the energy of the jet
B)
ratio of the actual power produced by the turbine to the energy actually supplied by the turbine
C)
Both (A) and (B)
D)
ratio of the actual work available at the turbine to the energy imparted to the wheel

Correct Answer :   ratio of the actual work available at the turbine to the energy imparted to the wheel

A)
weight
B)
impulse
C)
Can Not Say
D)
None of the above

Correct Answer :   weight

17 .
If Hg is the gross or total head and hf is the head lost due to friction, then net or effective head (H) is given by
A)
H = Hg - hf
B)
H = Hg/hf
C)
H = Hg x hf
D)
H = Hg + hf

Correct Answer :   H = Hg - hf

A)
2 to 4
B)
4 to 8
C)
8 to l6
D)
16 to 24

Correct Answer :   4 to 8

A)
directly proportional to diameter of its impeller
B)
inversely proportional to diameter of its impeller
C)
directly proportional to (diameter)² of its impeller
D)
inversely proportional to (diameter)² of its impeller

Correct Answer :   directly proportional to (diameter)² of its impeller


Explanation : Discharge of a centrifugal pump is directly proportional to (Diameter)^2 of its impeller.

Head of a centrifugal pump is directly proportional to (Diameter)^2 of its impeller.

Power Developed of a centrifugal pump is directly proportional to (Diameter)^4 of its impeller.

A)
develops unit power under unit head
B)
develops unit power under unit speed
C)
delivers unit discharge under unit head
D)
delivers unit discharge under unit speed

Correct Answer :   develops unit power under unit head

A)
efficiency will be low
B)
no flow will take place
C)
cavitation will be formed
D)
excessive power will be consumed

Correct Answer :   cavitation will be formed

A)
at full load
B)
corresponding to maximum overload permissible
C)
at which there will be no damage to the runner
D)
at which the turbine will run freely without load

Correct Answer :   at which the turbine will run freely without load

A)
high speed pump with radial flow at outlet
B)
slow speed pump with radial flow at outlet
C)
high speed pump with axial flow at outlet
D)
medium speed pump with radial flow at outlet

Correct Answer :   slow speed pump with radial flow at outlet

A)
reduces the discharge of a turbine
B)
causes noise and vibration of various parts
C)
causes sudden drop in power output and efficiency
D)
All of the above

Correct Answer :   All of the above

A)
175.4 r.p.m.
B)
215.5 r.p.m.
C)
241.5 r.p.m.
D)
275.4 r.p.m

Correct Answer :   241.5 r.p.m.

A)
True
B)
False
C)
Can Not Say
D)
None of the above

Correct Answer :   True

A)
Jonval turbine
B)
Furneyron turbine
C)
Pelton wheel
D)
Thomson's turbine

Correct Answer :   Pelton wheel

A)
Air lift pump
B)
Centrifugal pump
C)
Reciprocating pump
D)
Jet pump

Correct Answer :   Jet pump

A)
Nuclear power
B)
Hydroelectric power
C)
Thermal power
D)
Roto dynamic power

Correct Answer :   Hydroelectric power


Explanation : The energy from the energy of water is also called hydro power. The electric power so obtained is known as hydroelectric power.

A)
Elastic Energy
B)
Mechanical Energy
C)
Kinetic Energy
D)
Potential Energy

Correct Answer :   Mechanical Energy


Explanation : The kinetic and potential energies produced are converted to some useful mechanical energy. This part of energy is available to the turbine shaft.

A)
Outward flow turbine
B)
Mixed flow turbine
C)
Inward flow turbine
D)
Radial flow turbine

Correct Answer :   Outward flow turbine


Explanation : In a Fourneyron turbine, the flow is centrifugal type. The flow is outwards from the centre to the periphery.

A)
7
B)
6
C)
5
D)
4

Correct Answer :   5


Explanation : There are five types of reaction turbines namely VLH, Francis, Kaplan, Tyson, Gorolov helical turbine.

A)
allow the water to enter the runner without shock
B)
allow the water to flow over them, without forming eddies
C)
allow the required quantity of water to enter the turbine
D)
All of the above

Correct Answer :   All of the above

A)
energy supplied to the pump to the energy available at the impeller
B)
manometric head to the energy supplied by the impeller per kN of water
C)
energy available at the impeller to the energy supplied to the pump by the prime mover
D)
actual workdone by the pump to the energy supplied to the pump by the prime mover

Correct Answer :   energy available at the impeller to the energy supplied to the pump by the prime mover

A)
Correct
B)
Incorrect
C)
Can Not Say
D)
None of the above

Correct Answer :   Incorrect

37 .
Which of the following statement is correct ?
A)
In an impulse turbine, the water impinges on the buckets with pressure energy.
B)
In a reaction turbine, the water glides over the moving vanes with kinetic energy.
C)
In a reaction turbine, the pressure of the flowing water increases after gliding over the vanes.
D)
In an impulse turbine, the pressure of the flowing water remains unchanged and is equal to atmospheric pressure.

Correct Answer :   In an impulse turbine, the pressure of the flowing water remains unchanged and is equal to atmospheric pressure.

A)
to store pressure energy which may be supplied to a machine later on
B)
to lift larger load by the application of a comparatively much smaller force
C)
to increase the intensity of pressure of water by means of energy available from a large quantity of water at a low pressure
D)
All of the above

Correct Answer :   to lift larger load by the application of a comparatively much smaller force

A)
0.15 to 0.3
B)
0.4 to 0.5
C)
0.6 to 0.9
D)
1 to 1.5

Correct Answer :   0.15 to 0.3

A)
V₁ / V₁-V₂
B)
V₁-V₂ / V₁
C)
V₁² / V₁²-V₂²
D)
V₁²-V₂² / V₁²

Correct Answer :   V₁²-V₂² / V₁²

A)
inward flow impulse turbine
B)
outward flow impulse turbine
C)
tangential flow impulse turbine
D)
inward flow reaction turbine

Correct Answer :   tangential flow impulse turbine

A)
the wheel runs entirely by the weight of water
B)
the wheel runs partly by the weight of water and partly by the impulse of water
C)
the wheel runs entirely by the impulse of water
D)
None of the above

Correct Answer :   the wheel runs entirely by the impulse of water

43 .
The specific speed of a centrifugal pump may be defined as the speed of an imaginary pump, identical with the given pump, which will discharge one litre of water, while it is being raised through a head of one metre.
A)
True
B)
False
C)
Can Not Say
D)
None of the above

Correct Answer :   True

A)
Kaplan turbine
B)
Pelton wheel with one nozzle
C)
Francis turbine
D)
Pelton wheel with two or more nozzles

Correct Answer :   Pelton wheel with one nozzle

A)
Reciprocating pump
B)
Axial flow pump
C)
Mixed flow pump
D)
Centrifugal pump

Correct Answer :   Reciprocating pump

A)
1.2 times
B)
equal to
C)
1.8 times
D)
double

Correct Answer :   1.2 times

A)
high discharge
B)
low head of water
C)
medium head of water
D)
high head of water

Correct Answer :   high head of water

A)
Gear pump
B)
Screw pump
C)
Plunger pump
D)
Cam and piston pump

Correct Answer :   Plunger pump

A)
using stainless steel runner of the turbine
B)
providing highly polished blades to the runner
C)
installing the turbine below the tail race level
D)
All of the above

Correct Answer :   All of the above

A)
have identical velocities
B)
are identical in shape, but differ only in size
C)
have identical forces
D)
are equal in size and shape

Correct Answer :   are identical in shape, but differ only in size

A)
mechanical
B)
overall
C)
hydraulic
D)
None of the above

Correct Answer :   mechanical

A)
sum
B)
product
C)
difference
D)
None of the above

Correct Answer :   difference

A)
to run the turbine full
B)
to transport water to downstream
C)
to prevent air to enter the turbine
D)
to increase the head of water by an amount equal to the height of the runner outlet above the tail race

Correct Answer :   to increase the head of water by an amount equal to the height of the runner outlet above the tail race

A)
directly proportional
B)
inversely proportional
C)
Both (A) and (B)
D)
None of the above

Correct Answer :   directly proportional

A)
sum of actual discharge and the theoretical discharge
B)
difference of theoretical discharge and the actual discharge
C)
ratio of actual discharge to the theoretical discharge
D)
product of theoretical discharge and the actual discharge

Correct Answer :   difference of theoretical discharge and the actual discharge

A)
Yes
B)
No
C)
Can Not Say
D)
None of the above

Correct Answer :   Yes

58 .
Theoretical power required (in watts) to drive a reciprocating pump is (where w = Specific weight of liquid to be pumped in N/m3, Q = Discharge of the pump in m3/s, Hs = Suction head in metres, and Hd = Delivery head in metres)
A)
wQHs
B)
wQHd
C)
wQ(Hs - Hd)
D)
wQ(Hs + Hd)

Correct Answer :   wQ(Hs + Hd)

A)
24.8 r.p.m.
B)
48.2 r.p.m
C)
82.4 r.p.m.
D)
248 r.p.m

Correct Answer :   82.4 r.p.m.

A)
give high discharge
B)
pump viscous fluids
C)
produce high heads
D)
All of the above

Correct Answer :   produce high heads

A)
five times
B)
four times
C)
three times
D)
double

Correct Answer :   five times

A)
Kaplan turbine
B)
Pelton wheel
C)
Francis turbine
D)
None of the above

Correct Answer :   Pelton wheel

A)
1 to 1.5
B)
0.6 to 0.9
C)
0.4 to 0.5
D)
0.15 to 0.3

Correct Answer :   0.6 to 0.9

A)
Condensers
B)
Pulverizers
C)
Kinetic machinery
D)
Roto-dynamic machinery

Correct Answer :   Roto-dynamic machinery


Explanation : Hydraulic Machines use the principle of rotation of blades to alter the speed of water. Hence fall under roto dynamic machinery.

A)
Turgo turbine
B)
Screw Turbine
C)
Reaction turbine
D)
Impulse Turbine

Correct Answer :   Reaction turbine


Explanation : Francis turbine is a reaction turbine as it changes the pressure of water through its process. Hence it cannot be an impulse turbine.

A)
Reaction turbines
B)
Impulse turbines
C)
Kinetic turbines
D)
Reactive turbines

Correct Answer :   Reaction turbines


Explanation : Reaction turbines which act on water try to change the pressure of the water through its motion.

A)
Impulse turbines
B)
Reaction turbines
C)
Kinetic turbines
D)
Axial flow turbines

Correct Answer :   Impulse turbines


Explanation : In Impulse turbines, potential energy is utilized to convert as kinetic energy thereby changing the velocity of the water through its process.

A)
Hydraulic ram
B)
Hydraulic accumulator
C)
Hydraulic intensifier
D)
Hydraulic torque converter

Correct Answer :   Hydraulic torque converter

A)
dynamic similarity
B)
geometric similarity
C)
kinematic similarity
D)
None of the above

Correct Answer :   geometric similarity

A)
Correct
B)
Incorrect
C)
Can Not Say
D)
None of the above

Correct Answer :   Correct

71 .
The force exerted by a jet of water impinging normally on a plate which due to the impact of jet, moves in the direction of jet with a velocity v is
A)
wa (V-v) / g
B)
wa (V-v) / 2g
C)
wa (V-v)² / g
D)
wa (V-v)² / 2g

Correct Answer :   wa (V-v)² / g

A)
positive
B)
negative
C)
Can Not Say
D)
None of the above

Correct Answer :   positive

A)
parallel
B)
perpendicular
C)
Can Not Say
D)
None of the above

Correct Answer :   parallel

A)
two jets
B)
two runners
C)
four jets
D)
four runners

Correct Answer :   two runners

A)
axially
B)
radially
C)
Can Not Say
D)
None of the above

Correct Answer :   radially

A)
speed and head of water
B)
speed and power developed
C)
discharge and power developed
D)
speed, power developed and head of water

Correct Answer :   speed, power developed and head of water

A)
double
B)
three-fourth
C)
one-half
D)
one-fourth

Correct Answer :   one-half

80 .
The relation between hydraulic efficiency (ηh), mechanical efficiency (ηm) and overall efficiency (ηo) ) is
A)
ηo = ηh x ηm
B)
ηm = ηo x ηh
C)
ηh = ηo x ηm
D)
None of the above

Correct Answer :   ηo = ηh x ηm

A)
2 to 4
B)
4 to 8
C)
8 to l6
D)
16 to 24

Correct Answer :   16 to 24

A)
Tube Turbine
B)
Pelton Turbine
C)
Kaplan Turbine
D)
Francis turbine

Correct Answer :   Pelton Turbine


Explanation : Except Pelton remaining are reaction turbines, in impulse pressure energy is constant and only available energy is kinetic energy which is directly proportional to head.

A)
Pressure head + Static head
B)
Kinetic head + Static head
C)
Static head + Pressure head
D)
Pressure head + Kinetic head + Static head

Correct Answer :   Pressure head + Kinetic head + Static head


Explanation : Generally total is calculated as sum of pressure head, static head and kinetic head.

A)
100-200 meters
B)
70 -100 meters
C)
10-70 meters
D)
Above 200 meters

Correct Answer :   10-70 meters


Explanation : Kaplan turbine is reaction turbine and it operates at low head 10-70 meters and output power is 5-200 MW.

A)
20-50 meters
B)
15-2000 meters
C)
60-200 meters
D)
50-500 meters

Correct Answer :   15-2000 meters


Explanation : Pelton turbine is an impulse turbine only energy available is kinetic energy which is proportional to head, hence it requires high head. Theoretically there is no limit to max value of head.

A)
40-600 meters
B)
70-100 meters
C)
100-200 meters
D)
150-200 meters

Correct Answer :   40-600 meters


Explanation : Francis turbine is also reaction turbine but pressure energy is less when compared with Kaplan turbine. Hence head is between 40 and 600 meters.

A)
Kaplan turbine
B)
Tube turbine
C)
Pelton wheel
D)
Francis turbine

Correct Answer :   Kaplan turbine


Explanation : Kaplan is reaction turbine and its range of operation is between 10-70 meters which has output range between 5-200 MW.

A)
Overall efficiency
B)
Mechanical efficiency
C)
Volumetric efficiency
D)
Hydraulic efficiency

Correct Answer :   Hydraulic efficiency


Explanation : Hydraulic efficiency is defined as ratio between power given by water to runner of turbine and to the power supplied by water at inlet of the turbine.

A)
Mechanical efficiency
B)
Volumetric efficiency
C)
Electrical efficiency
D)
Hydraulic efficiency

Correct Answer :   Electrical efficiency


Explanation : Electrical efficiency is ratio of work output and electrical power input to electrical machine but turbine is a hydraulic machine which consists of only mechanical, volumetric and hydraulic efficiencies.

A)
Hydraulic efficiency
B)
Overall efficiency
C)
Volumetric efficiency
D)
Mechanical efficiency

Correct Answer :   Overall efficiency


Explanation : Overall efficiency is defined as ratio of power available at shaft of turbine to power supplied at the inlet of turbine which is also product of mechanical and hydraulic efficiency.

A)
Half
B)
Twice
C)
Thrice
D)
One quarter

Correct Answer :   Half


Explanation : Hydraulic efficiency is defined as ratio between power given by water to runner of turbine and to the power supplied by water at inlet of the turbine. This efficiency will be maximum when differentiating it with “u” and it is obtained as u=v/2.

A)
to break the jet of water
B)
to change the direction of runner
C)
to bring the runner to rest in a short time
D)
None of the above

Correct Answer :   to bring the runner to rest in a short time

94 .
The water in a jet propelled boat is drawn through the openings facing the direction of motion of the boat. The efficiency of propulsion is given by
A)
2V / Vr-v
B)
2V / Vr+v
C)
V / Vr-v
D)
V / Vr+v

Correct Answer :   2V / Vr+v

95 .
The ratio of the normal force of jet of water on a plate inclined at an angle of 30° as compared to that when the plate is normal to jet, is
A)
1
B)
1/2
C)
√2
D)
1/√2

Correct Answer :   1/2

A)
proportional to speed of impeller
B)
proportional to diameter of impeller
C)
proportional to diameter and speed of impeller
D)
None of the above

Correct Answer :   proportional to diameter and speed of impeller

A)
(1+cos k)/2 where k is outlet blade angle
B)
(2+cos k)/2 where k is outlet blade angle
C)
(3+cos k)/2 where k is outlet blade angle
D)
(4+cos k)/2 where k is outlet blade angle

Correct Answer :   (1+cos k)/2 where k is outlet blade angle


Explanation : Hydraulic efficiency is defined as ratio between power given by water to runner of turbine and to the power supplied by water at inlet of the turbine. Its maximum value is obtained by replacing u=v/2 and it is (1+cos k)/2 where k is outlet blade angle

A)
Hydraulic efficiency
B)
Volumetric efficiency
C)
Overall efficiency
D)
Mechanical efficiency

Correct Answer :   Volumetric efficiency


Explanation : Volumetric efficiency is ratio between volume of water actually striking the runner of turbine and volume of water supplied to the turbine.

A)
Mixed flow pump
B)
Centrifugal pump
C)
Reciprocating pump
D)
Axial flow pump

Correct Answer :   Axial flow pump

A)
increases
B)
decreases
C)
remains same
D)
None of the above

Correct Answer :   increases

A)
increases
B)
decreases
C)
Can Not Say
D)
None of the above

Correct Answer :   increases

A)
L.A.N
B)
2 L.A.N
C)
L.A.N / 60
D)
2 L.A.N / 60

Correct Answer :   2 L.A.N / 60

A)
depends
B)
does not depend
C)
Can Not Say
D)
None of the above

Correct Answer :   depends

A)
Pelton wheel
B)
Francis turbine
C)
Kaplan turbine
D)
None of the above

Correct Answer :   Kaplan turbine

A)
actual work available at the turbine to the energy imparted to the wheel
B)
power produced by the turbine to the energy actually supplied by the turbine
C)
workdone on the wheel to the energy (or head of water) actually supplied to the turbine
D)
None of the above

Correct Answer :   power produced by the turbine to the energy actually supplied by the turbine

A)
two
B)
four
C)
six
D)
eight

Correct Answer :   six

A)
Q = π.b.Vf
B)
Q = π.D.Vf
C)
Q = D.b.Vf
D)
Q = π.D.b.Vf

Correct Answer :   Q = Ï€.D.b.Vf

A)
manometric head
B)
static head
C)
kinetic head
D)
velocity head

Correct Answer :   manometric head

A)
energy transfer machines
B)
power absorbing machines
C)
power developing machines
D)
energy generating machines

Correct Answer :   energy transfer machines

A)
Workdone per kN of water - Losses within the impeller
B)
Energy per kN at outlet of impeller - Energy per kN at inlet of impeller
C)
Suction lift + Loss of head in suction pipe due to friction + Delivery lift + Loss of head in delivery pipe due to friction + Velocity head in the delivery pipe
D)
All of the above

Correct Answer :   All of the above

A)
25° to 30°
B)
20° to 25°
C)
15° to 20°
D)
10° to 15°

Correct Answer :   20° to 25°

A)
unit speed
B)
normal speed
C)
specific speed
D)
None of the above

Correct Answer :   specific speed

A)
overall efficiency
B)
volumetric efficiency
C)
manometric efficiency
D)
mechanical efficiency

Correct Answer :   volumetric efficiency

A)
Measure discharge of flow
B)
Angle of deflection of jet
C)
Flow of water along blades of turbine
D)
Flow of water, measure of discharge, angle of deflection

Correct Answer :   Flow of water, measure of discharge, angle of deflection


Explanation : By using velocity triangles we can determine discharge of flow, angle of deflection of jet and to measure relative velocity of jet with respect to speed of wheel.

A)
Pelton turbine
B)
Kaplan turbine
C)
Francis turbine
D)
Propeller turbine

Correct Answer :   Pelton turbine


Explanation : In Pelton turbine each blade has same angular velocity and same linear speed unlike Francis and Kaplan turbines.

A)
Correct
B)
Incorrect
C)
Can Not Say
D)
None of the above

Correct Answer :   Correct

A)
0.50 to 0.65
B)
0.65 to 0.75
C)
0.75 to 0.85
D)
0.85 to 0.90

Correct Answer :   0.85 to 0.90

A)
ratio of the actual work available at the turbine to the energy imparted to the wheel
B)
ratio of the work done on the wheel to the energy of the jet
C)
ratio of the actual power produced by the turbine to the energy actually supplied by the turbine
D)
None of the above

Correct Answer :   ratio of the work done on the wheel to the energy of the jet

A)
0.26
B)
0.36
C)
0, 46
D)
0.56

Correct Answer :   0, 46

A)
smoothen the flow
B)
reduce suction head
C)
increase delivery head
D)
reduce acceleration head

Correct Answer :   reduce acceleration head

A)
geometric similarity
B)
dynamic similarity
C)
kinematic similarity
D)
None of the above

Correct Answer :   dynamic similarity

A)
increases
B)
decreases
C)
remains same
D)
None of the above

Correct Answer :   decreases

A)
Screw pump
B)
Air lift pump
C)
Centrifugal pump
D)
Reciprocating pump

Correct Answer :   Screw pump

A)
Correct
B)
Incorrect
C)
Can Not Say
D)
None of the above

Correct Answer :   Correct

A)
the suction pressure should be low
B)
the delivery pressure should be low
C)
the suction pressure should be high
D)
the delivery pressure should be high

Correct Answer :   the suction pressure should be high

A)
actual work available at the turbine to energy imparted to the wheel
B)
power produced by the turbine to the energy actually supplied by the turbine
C)
Both (A) and (B)
D)
workdone on the wheel to the energy (or head of water) actually supplied to the turbine

Correct Answer :   workdone on the wheel to the energy (or head of water) actually supplied to the turbine

A)
a mixed flow
B)
an inward flow
C)
an axial flow
D)
an outward flow

Correct Answer :   an inward flow

A)
Jet pump
B)
Air-lift pump
C)
Centrifugal pump
D)
Reciprocating pump

Correct Answer :   Jet pump

A)
Jet pump
B)
Centrifugal pump
C)
Reciprocating pump
D)
Air lift pump

Correct Answer :   Air lift pump

A)
delivery pipe is long and pump is running at high speeds
B)
suction pipe is short and pump is running at low speeds
C)
suction pipe is long and delivery pipe is short and the pump is running at high speeds
D)
suction pipe is short and delivery pipe is long and the pump is running at low speeds

Correct Answer :   suction pipe is long and delivery pipe is short and the pump is running at high speeds

A)
a mixed flow
B)
an axial flow
C)
an outward flow
D)
an inward flow

Correct Answer :   an outward flow

134 .
The discharge through a turbine is
A)
directly proportional to H1/2
B)
inversely proportional to H1/2
C)
directly proportional to H3/2
D)
inversely proportional to H3/2

Correct Answer :   directly proportional to H1/2

A)
Pelton wheel
B)
Kaplan turbine
C)
Turgo turbine
D)
Girad turbine

Correct Answer :   Kaplan turbine

A)
pressure
B)
strain
C)
kinetic
D)
None of the above

Correct Answer :   pressure

A)
energy supplied to the pump to the energy available at the impeller
B)
manometric head to the energy supplied by the impeller per kN of water
C)
energy available at the impeller to the energy supplied to the pump by the prime mover
D)
actual workdone by the pump to the energy supplied to the pump by the prime mover

Correct Answer :   actual workdone by the pump to the energy supplied to the pump by the prime mover

A)
volute casing
B)
vortex casing
C)
volute casing with guide blades
D)
any one of these

Correct Answer :   any one of these

A)
have identical forces
B)
are equal in size and shape
C)
have identical velocities
D)
are identical in shape, but differ only in size

Correct Answer :   have identical velocities

A)
Zero
B)
x- component of V(r2) – blade velocity
C)
x- component of V (r2) + blade velocity
D)
Blade velocity – x- component of V (r2)

Correct Answer :   x- component of V(r2) – blade velocity


Explanation : By constructing velocity triangle we come to know that whirl velocity of jet is equal in magnitude to that of x- component of V r2 – blade velocity.

A)
165 degrees
B)
185 degrees
C)
200 degrees
D)
225 degrees

Correct Answer :   165 degrees

A)
Volumetric efficiency
B)
Hydraulic efficiency
C)
Overall efficiency
D)
Mechanical efficiency

Correct Answer :   Hydraulic efficiency


Explanation : Hydraulic efficiency is defined as ratio between power given by water to runner of turbine and to the power supplied by water at inlet of the turbine.

A)
Hydraulic efficiency
B)
Volumetric efficiency
C)
Overall efficiency
D)
Mechanical efficiency

Correct Answer :   Overall efficiency


Explanation : Overall efficiency is defined as ratio of power available at shaft of turbine to power supplied at the inlet of turbine which is also product of mechanical and hydraulic efficiency.

A)
Density of liquid
B)
Volume of liquid
C)
Specific density of liquid
D)
Specific gravity of liquid

Correct Answer :   Density of liquid


Explanation : Overall efficiency is defined as ratio of power available at shaft of turbine to power supplied at the inlet of turbine which is also product of mechanical and hydraulic efficiency. Its expression is given by p/ (k*g*q*h) where k is density of liquid.

A)
2(V1-u)[1+cos k]u/V1*V1
B)
2(V1+u)[1+cos k]u/V1*V1
C)
2(V1-u)[1-cos k]u/V1*V1
D)
2(V1+u)[1+cos k]u/V1*V1

Correct Answer :   2(V1-u)[1+cos k]u/V1*V1


Explanation : Hydraulic efficiency is ratio of power delivered to runner to power supplied at inlet of turbine upon substituting the mathematical terms we get expression as follows.

Where, V1=inlet jet velocity, u=blade velocity, k=outlet blade angle

A)
Axial direction
B)
Tangential direction
C)
Both (A) and (B)
D)
Radial direction

Correct Answer :   Radial direction


Explanation : The name itself indicates the type of flow that is radial direction but the thing that is unknown is whether it is radially inward or outwards.

A)
P1*b1*Vf1
B)
P2*b2*Vf2
C)
P1*b2*Vf2
D)
Both P1*b1*Vf1 & P2*b2*Vf2

Correct Answer :   Both P1*b1*Vf1 & P2*b2*Vf2


Explanation : Discharge of radial flow reaction turbine is product of perimeter of runner, thickness, whirl velocity, at inlet as well as outlet runner vanes.

Where, P1=perimeter of runner at inlet, P2=perimeter of runner at outlet, b=thickness and Vf=flow velocity.

A)
Runner
B)
Guide mechanism
C)
Casing
D)
Drafting

Correct Answer :   Guide mechanism


Explanation : Guide vanes are placed around the runner to regulate the flow and to provide shock less entry at inlet to runner.

A)
Variable velocity
B)
Variable acceleration
C)
Constant velocity
D)
Constant acceleration

Correct Answer :   Constant velocity


Explanation : Area of spiral structure gradually decreases because as discharge decreases correspondingly area also decreases. So, runner will rotate with constant velocity.

A)
Lesser
B)
Equal
C)
Greater
D)
Constant

Correct Answer :   Lesser


Explanation : In general, the exit of runner has a low pressure compared to the atmospheric pressure.

A)
Runner
B)
Casing
C)
Draft tube
D)
Guide mechanism

Correct Answer :   Draft tube


Explanation : Draft is a pipe of gradually increasing area, as water leaving runner has less pressure, draft tube will increase pressure energy of water by decreasing its velocity.

A)
Casing and penstocks
B)
Runner and penstocks
C)
Runner and draft tube
D)
Casing and runner

Correct Answer :   Casing and runner


Explanation : Casing and runner are completely covered by water as it is a reaction turbine in which pressure energy is predominant.

A)
runner
B)
casing
C)
draft tube
D)
guide wheel

Correct Answer :   casing


Explanation : The water from penstocks enters the casing which is spiral in shape in which the area of cross section of casing decreases gradually.

A)
Inward flow turbine
B)
Tangential flow turbine
C)
Turbulent low inward flow
D)
Outward flow turbine

Correct Answer :   Outward flow turbine


Explanation : If the water in the runner flows from inwards to outwards, then such type of turbine is said to be outward radial flow turbine.

A)
kinetic energy and pressure energy
B)
kinetic energy and potential energy
C)
potential energy and pressure energy
D)
gravitational energy and potential energy

Correct Answer :   kinetic energy and pressure energy


Explanation : Reaction turbine is a kind of turbine in which the water at inlet of the turbine possesses both kinetic energy and pressure energy.

A)
Discharge
B)
Flow ratio
C)
Speed ratio
D)
Radial discharge

Correct Answer :   Flow ratio


Explanation : Flow ratio is known as ratio of tangential wheel at inlet to given velocity of jet and it is scalar quantity.

A)
Flow ratio
B)
Speed ratio
C)
Degree of reaction
D)
Hydraulic efficiency

Correct Answer :   Degree of reaction


Explanation : This is just a formula and it is scalar quantity because it is ratio of two changes of energies.

A)
1- cot x /2(cot x –cot y)
B)
1+ cot x /2(cot x –cot y)
C)
1- cot x /2(cot x +cot y)
D)
1+ cot x /2(cot x +cot y)

Correct Answer :   1- cot x /2(cot x –cot y)


Explanation : Because for reaction turbine Vw2=0 and V2=Vf2, there is also no much change in velocity of flow implies that Vf1=Vf2 by substituting these values, we get it.

A)
Vane angle
B)
Heat rejection
C)
Moving fluid
D)
Increase in temperature

Correct Answer :   Moving fluid


Explanation : The Pelton wheel extracts energy from moving of fluid. When the fluid flows through the Pelton wheel, a kinetic energy is developed. This kinetic energy is extracted from the moving fluid.

A)
Same pressure
B)
Volumetric change
C)
Pressure independent
D)
Pressure change

Correct Answer :   Pressure change


Explanation : In impulse turbines, there is pressure change in blades of the turbine. There is pressure change that is developed in fluid or gas in the turbine blades. The turbine blades are in stationary condition.

A)
Increases
B)
Decreases
C)
Independent
D)
None of the above

Correct Answer :   Decreases


Explanation : In an inward flow reaction turbine the discharge of fluid decreases. Thus, making it different from an outward flow reaction turbine.

A)
Radially inward
B)
Axial direction
C)
Radial direction
D)
Radially outward

Correct Answer :   Radially inward


Explanation : The name itself indicates that flow is in radial direction and flowing from outer periphery towards center.

A)
Axial turbine
B)
Francis turbine
C)
Pelton wheel
D)
Kaplan turbine

Correct Answer :   Francis turbine


Explanation : Pelton is impulse a turbine, Kaplan is axial flow turbine and Francis is an inward flow reaction turbine.

A)
Axial direction
B)
Radially outward
C)
Radially inward
D)
Radial direction

Correct Answer :   Radially inward


Explanation : The name itself indicates the type of flow that is radial direction but the thing that is unknown is whether it is radially inward or outwards.

A)
(P1-n*t)*b1*Vf1
B)
(P2-n*t)*b2*Vf2
C)
(P1-n*t)*b2*Vf2
D)
Both (P1-n*t)*b1*Vf1 & (P2-n*t)*b2*Vf2

Correct Answer :   Both (P1-n*t)*b1*Vf1 & (P2-n*t)*b2*Vf2


Explanation : Discharge of radial flow reaction turbine is product of perimeter of runner, thickness, whirl velocity, at inlet as well as outlet runner vanes. If n blades of thickness t is considered then discharge is (P1-n*t)*b1*Vf1.

Where, P1=perimeter of runner at inlet, P2=perimeter of runner at outlet, b=width, Vf=flow velocity, n=number of blades and t=thickness of blades

A)
Flow ratio
B)
Speed ratio
C)
Radial inlet discharge
D)
Radial outlet discharge

Correct Answer :   Radial outlet discharge


Explanation : If angle made by absolute velocity with its tangent is 90 degrees and component of whirl is zero at outlet in radial flow reaction then total velocity will be flow velocity.

A)
Inward flow reaction turbine
B)
Impulse turbine
C)
Axial flow turbine
D)
Outward flow reaction turbine

Correct Answer :   Inward flow reaction turbine


Explanation : In an inward reaction flow turbine, wheel moves with the constant speed.

A)
Axial and then radial
B)
Radial and then axial
C)
Axial and then tangential
D)
Tangential and then axial

Correct Answer :   Radial and then axial


Explanation : Francis turbine is radial flow reaction turbine. Though the water enters the turbine tangentially, it enters the runner radially inward and flows outward along the axis of the runner.

A)
To prevent leakage from the turbine
B)
To reduce material costs in order to make the turbine more economical
C)
To ensure constant velocity of water during runner entry
D)
To prevent loss of efficiency of the turbine due to impulsive forces caused by extra area

Correct Answer :   To ensure constant velocity of water during runner entry


Explanation : The primary purpose of the gradual decrease in area is so that the runner sees constant velocity of water at each point of entry. Absence of this may lead to inefficiency. The spiral casing is used to prevent leakage from the turbine but the gradual decrease in area is not for that reason.

A)
Slow Runner
B)
Fast Runner
C)
Medium Runner
D)
None of the above

Correct Answer :   Fast Runner


Explanation : Considering the velocity diagram of Francis turbine at the inlet for a fast runner, vane angle is an obtuse angle. Whereas, it is right angle for medium runner and an acute angle for a slow runner.

A)
Vw1 / u1
B)
Vr1 / u1
C)
Vr1 / Vw1
D)
Vf1 / Vw1

Correct Answer :   Vw1 / u1


Explanation : In medium runner, Vf1 = Vr1 & Vw1 = u1. Vw1 and u1 are along the same direction, hence that cannot be written as tan (α1).

A)
Overall efficiency
B)
Mechanical efficiency
C)
Volumetric efficiency
D)
Hydraulic efficiency

Correct Answer :   Hydraulic efficiency


Explanation : The definition of Hydraulic efficiency in a Francis turbine states that it is the ratio between the Runner power to the shaft power. Hence, the correct option is Hydraulic efficiency.

A)
Overall efficiency
B)
Volumetric efficiency
C)
Hydraulic efficiency
D)
Mechanical efficiency

Correct Answer :   Overall efficiency


Explanation : The definition of Overall efficiency in a Francis turbine states that it is the ratio between the Shaft power to the Water power. Hence, the correct option is Overall efficiency.

A)
60
B)
70
C)
80
D)
90

Correct Answer :   80


Explanation : The definition of Hydraulic efficiency in a Francis turbine states that it is the ratio between the Runner power to the shaft power. If input water power is 1.25 times the runner power, the runner power is 1/1.25 = 0.8 Times the water power. Hence, hydraulic efficiency = 80%.

175 .
The volume flow rate of water in 10 m³/s at an available head of 60 m (g = 10 m/s³). Find the shaft power (in MW) if the overall efficiency of the turbine is 90%.
A)
0.54
B)
5.4
C)
54
D)
540

Correct Answer :   5.4


Explaination : The overall efficiency of a Francis turbine is given by ηo = shaft power/ ρQgH. Substituting the given values in this equation, we get shaft power = 5.4 MW.

A)
Radial and then axial
B)
Axial and then axial
C)
Tangential and then axial
D)
Tangential and then radial

Correct Answer :   Axial and then axial


Explanation : The Kaplan turbine is an axial flow reaction turbine. The water inlet is axial and the water outlet is axial too.

A)
Kaplan Turbine
B)
Francis turbine
C)
Pelton turbine
D)
Propeller Turbine

Correct Answer :   Francis turbine


Explanation : In a Kaplan turbine, the guide vanes are adjustable and not fixed to the hub of the turbine. Francis and Pelton turbines are not low head turbines. In a propeller turbine, the guide vanes are fixed to the hub of the turbine.

A)
Kaplan turbine
B)
Steam turbine
C)
Pelton turbine
D)
Francis turbine

Correct Answer :   Kaplan turbine


Explanation : As the head for Kaplan turbine is low, the discharge of water through the turbine is high and hence, blade resistance should be low. That’s why Kaplan turbine will have the lowest number of blades.

A)
Overall efficiency
B)
Volumetric efficiency
C)
Mechanical efficiency
D)
Hydraulic efficiency

Correct Answer :   Hydraulic efficiency


Explanation : The definition of Hydraulic efficiency in a Kaplan turbine states that it is the ratio between the Runner power to the shaft power. Hence, the correct option is Hydraulic efficiency.

A)
70.71
B)
80.81
C)
90.91
D)
100.00

Correct Answer :   90.91


Explanation : The definition of Hydraulic efficiency in a Kaplan turbine states that it is the ratio between the Runner power to the shaft power. If input water power is 1.10 times the runner power, the runner power is 1/1.10 = 0.90909 Times the water power. Hence, hydraulic efficiency = 90.91%.