021.10 PISTON ENGINES Flashcards

1
Q

The camshaft of a piston engine rotates at (the) (same/half/twice) ​the speed of the crankshaft.

A

The camshaft of a piston engine rotates at (half) the speed of the crankshaft.

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2
Q

State which of the following comprises the crank assembly:

  • crankcase
  • crankshaft
  • valve springs
  • pistons
  • connecting rods
A

State which of the following comprises the crank assembly:

  • crankcase
  • crankshaft
  • valve springs
  • pistons
  • connecting rods
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3
Q

The power cycle process in a piston engine is (intermittent/continuous) and theoretically the combustion occurs at constant (volume/pressure)​.

A

The power cycle process in a piston engine is (intermittent) and theoretically the combustion occurs at constant (volume).

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4
Q

Ignition occurs in each cylinder of a four-stroke engine (before/behind) TDC at (each/each second) crankshaft revolution.

A

Ignition occurs in each cylinder of a four-stroke engine (before) TDC at (each second) crankshaft revolution.

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5
Q

Diesel engine have a (lower/higher) compresssion ratio and produce (less/more) maximum power as compared to petrol engines.

A

Diesel engine have a (higher) compresssion ratio and produce (less) maximum power as compared to petrol engines.

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6
Q

The higher the compresion ratio, the (lower/higher) the octane rating required.

A

The higher the compresion ratio, the (higher) the octane rating required.

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7
Q

A (thermocouple/bimetallic strip/bourdon tube) is used to monitor the cylinder head temperature.

A

A (thermocouple) is used to monitor the cylinder head temperature.

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8
Q

For a piston engine, the chemically correct fuel/air ration is 1:(…)​.

A

For a piston engine, the chemically correct fuel/air ration is 1:(15).

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9
Q

The richness of a fuel/air mixture ratio is the (mass/volume) of fuel to the (mass/volume) ​of the air.

A

The richness of a fuel/air mixture ratio is the (mass) of fuel to the (mass) of the air.

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10
Q

Concerning the twisting force acting on a propeller blade, the centrifugal twisting force tends to (increase/decrease) the blade angle and the aerodynamic twisting force tends to (increase/decrease) the blade angle.

A

Concerning the twisting force acting on a propeller blade, the centrifugal twisting force tends to (decrease) the blade angle and the aerodynamic twisting force tends to (increase) ​the blade angle.

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