ALL ABOUT BASIC ENGINE Flashcards

1
Q

The name is derived (the back and forth) movement of the piston which produces mechanical energy operates on the basic principle of converting chemical energy (FUEL DN AIR) to mechanical energy

A

Reciprocating engine

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2
Q

Most popular reciprocating engine used on small aircraft. It has a small and lightweight crank case

A

Opposed engine

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3
Q

Compresses fuel and air mixture

A

Piston

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4
Q

Simply connect piston and crankshaft

A

Connecting rod

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5
Q

Convert the energy from piston into rotary motion

A

Crankshaft

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6
Q

Introduction of fuel and air mixture

A

Intake valve

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7
Q

Removal of burned gases

A

Exhaust valve

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8
Q

For ignition

A

Sparkplug

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9
Q

the simplest of propeller designs and is associated with many light, piston engine aircraft. The angle of attack of is set at installation and cannot be changed during aircraft operation.

A

Fixed pitch propeller

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10
Q

a simple type of aircraft variable-pitch propeller where the blade angle can be adjusted between pre-set limits of fine and coarse pitch

A

Ground adjustable pitch propeller

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11
Q

the propeller blades are attached to the boss and their pitch can be altered via a hydraulic system. The blades are removable so if they incur damage, can be repaired without removal of the whole propellor.

A

Controllable pitch propeller

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12
Q

a type of variable pitch propeller that maintains a constant rotational speed by automatically adjusting blade pitch. They get the name constant speed because they can maintain a steady RPM while in flight.

A

Constant speed propeller

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13
Q

a pilot selectable feature of a constant speed or variable pitch propeller which allows the blade pitch to be decreased to a negative value. Negative pitch angles result in the thrust generated by the propeller being directed forward against the direction of motion of the aircraft.

A

Reverse speed propeller

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14
Q

to increase their angle of pitch by turning the blades to be parallel to the airflow. This minimizes drag from a stopped propeller following an engine failure in flight.

A

Feathering propeller

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15
Q

They are made to provide the correct amount of load on the engine during the test break-in period. The multi-blade design also provides extra cooling air flow during testing.

A

Test club propeller

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16
Q

Controls a mixture needle which restricts the amount of fuel flow in the float chamber Mixture adjustment required for changes in air density (changes in altitude)

A

Mixture knob

17
Q

Benefits of properly leaned engines

A

Better engine performance
Better fuel efficiency

18
Q

Disadvantages of improperly leaned engines: mixture too lean

A

High engine temperatures
Lower engine power output
Rough engine and can cause detoriation and Pre-Ignition

19
Q

Disadvantages of improperly leaned engines: Mixture too rich

A

Lower engine power output
High fuel consumption
Possible fouling of spark plugs

20
Q

Pre- Heats the air before it reaches the carburetor

A

Carburetor heat

21
Q

Application of Carburetor Heat

A

Reduction in engine power

If carburetor ice was present, there will be a slight increase in RPM

If carburetor ice was not present, RPM decrease and remain constant

22
Q

Contain large amount of carbon monoxide which is odorless and colorless gas.

A

Exhaust gases

23
Q

measures the temperature of gases at the exhaust manifold.

It can also be used for regulating the Fuel/Air Mixture

A

Exhaust gauge temperature

24
Q

Fuel system classification

A

Gravity feed system
Fuel pump system

25
Q

Air Cooling Design: Redirects air into the engine nacelles

A

Spinner

26
Q

Air cooling design: Redirects cold air to the parts of the engine which would not normally be cooled.

A

Baffles

27
Q

Air cooling design: Expand the surface area to improve cooling

A

Cooling fins

28
Q

Air cooling design: Pilot controlled air vents outside the engine to improve cooling

A

Cowl flaps

29
Q

Reducing pitch for better cooling
Reduce Power
Mixture - Rich
Keeping Oil levels high
Cowl Flaps - OPEN

A

Reducing temperature

30
Q

Engine Cooling
Engine lubrication
Piston sealing
Carrying away of contaminants

A

Functions of the oil system

31
Q

High viscosity
Low pour Points High flash point
Low carbon content
Oil system is vital to the “internal” cooling of the engine.

A

Properties of aircraft oil

32
Q

Sump
Oil Pump
Oil Cooler
Oil Filter
Pressure relief valve

A

Oil system parts

33
Q

attached to the under surface of the tank, acts as a trap for moisture and sediment. The water and sludge can be drained by manually opening the drain valve in the bottom of the sump. Most aircraft oil systems are equipped with the dipstick-type quantity gauge, often called a bayonet gauge.

A

Oil sump

34
Q

designed to supply oil under pressure to the parts of the engine that require lubrication, then circulate the oil through coolers as needed, and return the oil to the oil tank.

A

Oil pump

35
Q

helps keep the aircraft oil temperature from spiking while the engine runs. If the temperature begins to rise, the oil will be channeled through a heat exchanger which uses either air or fuel to lower the oil temperature.

A

Oil cooler

36
Q

essential components to maintain your aircraft’s engine. Just as the heart relies on clean arteries to function optimally, your engine relies on a clean oil supply

A

Oil filter

37
Q

a type of safety valve used to control or limit the pressure in a system; excessive pressure might otherwise build up and create a process upset, instrument or equipment failure, explosion, or fire.

A

Pressure relief valve