021.10 PISTON ENGINES Flashcards
The camshaft of a piston engine rotates at (the) (same/half/twice) the speed of the crankshaft.
The camshaft of a piston engine rotates at (half) the speed of the crankshaft.
State which of the following comprises the crank assembly:
- crankcase
- crankshaft
- valve springs
- pistons
- connecting rods
State which of the following comprises the crank assembly:
- crankcase
- crankshaft
- valve springs
- pistons
- connecting rods
The power cycle process in a piston engine is (intermittent/continuous) and theoretically the combustion occurs at constant (volume/pressure).
The power cycle process in a piston engine is (intermittent) and theoretically the combustion occurs at constant (volume).
Ignition occurs in each cylinder of a four-stroke engine (before/behind) TDC at (each/each second) crankshaft revolution.
Ignition occurs in each cylinder of a four-stroke engine (before) TDC at (each second) crankshaft revolution.
Diesel engine have a (lower/higher) compresssion ratio and produce (less/more) maximum power as compared to petrol engines.
Diesel engine have a (higher) compresssion ratio and produce (less) maximum power as compared to petrol engines.
The higher the compresion ratio, the (lower/higher) the octane rating required.
The higher the compresion ratio, the (higher) the octane rating required.
A (thermocouple/bimetallic strip/bourdon tube) is used to monitor the cylinder head temperature.
A (thermocouple) is used to monitor the cylinder head temperature.
For a piston engine, the chemically correct fuel/air ration is 1:(…).
For a piston engine, the chemically correct fuel/air ration is 1:(15).
The richness of a fuel/air mixture ratio is the (mass/volume) of fuel to the (mass/volume) of the air.
The richness of a fuel/air mixture ratio is the (mass) of fuel to the (mass) of the air.
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.
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.