Mechanical efficiency
Overall efficiency
Indicated thermal efficiency
Volumetric efficiency
B. Overall efficiency
Decreasing the density of intake air
Increasing the temperature of intake air
Increasing the pressure of intake air
Decreasing the pressure of intake air
Petrol, air and lubricating oil
Air and diesel
Petrol and lubricating oil
Petrol and air
Minimum temperature to which oil is heated in order to give off inflammable vapours in sufficient quantity to ignite momentarily when brought in contact with a flame
Temperature at which it solidifies or congeals
It catches fire without external aid
Indicated by 90% distillation temperature, i.e., when 90% of sample oil has distilled off
1 valve
2 valves
3 valves
4 valves
248 cm3
252 cm3
264 cm3
286 cm3
Increase
Decrease
Remain same
None of these
Thermal efficiency of diesel engine is about 34%
Theoretically correct mixture of air and petrol is approximately 15:1
High speed compression engines operate on dual combustion cycle
S.I. engines are quality governed engines
Vaporisation
Carburetion
Ionisation
Atomisation
Inlet valve closing after bottom dead centre
Inlet valve closing before bottom dead centre
Inlet valve opening before top dead centre
Exhaust valve closing after top dead centre
Using additives in the fuel
Increasing the compression ratio
Adherence to proper fuel specification
Avoidance of overloading
15 %
30 %
50 %
70 %
Clearance volume
Volumetric efficiency
Ignition time
Effective compression ratio
1 - rγ - 1
1 + rγ - 1
1 - (1/rγ - 1)
None of these
Not effected
Decrease
Increase
None of these
In compression ignition engines, detonation occurs near the beginning of combustion.
Since the fuel, in compression ignition engines, is injected at the end of compression stroke, therefore, there will be no pre-ignition.
To eliminate knock in compression ignition engines, we want to achieve auto-ignition not early and desire a long delay period.
In compression ignition engines, because of heterogeneous mixture, the rate of pressure rise is comparatively lower.
Compression starts at 35° after bottom dead center and ends at top dead center
Compression starts at bottom dead center and ends at top dead center
Compression starts at 10° before bottom dead center and, ends just before top dead center
May start and end anywhere
9 : 1
12 : 1
15 : 1
18 : 1
Equal to
Less than
Greater than
None of these
More
Less
Same
May be more or less depending on engine capacity
Diesel engines
Gas turbines
Petrol engines
Aircraft engines
The ratio of volumes of air in cylinder before compression stroke and after compression stroke
Volume displaced by piston per stroke and clearance volume in cylinder
Ratio of pressure after compression and before compression
Swept volume/cylinder volume
Fuel pump
Fuel injector
Governor
Carburettor
0.3 to 0.7 mm
0.2 to 0.8 mm
0.4 to 0.9 mm
0.6 to 1.0 mm
Morse test
Prony brake test
Motoring test
Heat balance test
Napthene
Tetra ethyl lead
Amyl nitrate
Hexadecane
It is properly designed
Best quality fuel is used
Cannot work as it is impossible
Flywheel size is proper
A supercharger
A centrifugal blower
A vacuum chamber
An injection tube
Otto cycle
Joule cycle
Rankine cycle
Stirling cycle
180°
125°
235°
200°
0
50
100
120