What's Your Knowledge In Propulsion Of Aircrafts?

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1. What is the Major purpose of the fins which are placed around the cylinder head of an air-cooled engine?

Explanation

The fins placed around the cylinder head of an air-cooled engine serve the major purpose of allowing heat to escape quickly. As air flows over the fins, it helps in dissipating the heat generated during the combustion process. This prevents the engine from overheating and ensures efficient cooling. By increasing the surface area available for heat transfer, the fins enhance the cooling capacity of the engine, allowing it to operate at optimal temperatures.

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About This Quiz
Whats Your Knowledge In Propulsion Of Aircrafts? - Quiz

Propulsion of Aircraft is an aircraft engine that generates a thrust, which is typically a propeller or a propulsive nozzle. These engines produce balance to drag of the... see moreairplane when the airplane is cruising and to exceed the drag of the airplane for the airplane to accelerate. How well do you understand the Propulsion of Aircraft? Find out by taking this quiz. see less

2. The basic function of the constant speed unit (CSU) in an aircraft propeller system is to?

Explanation

The constant speed unit (CSU) in an aircraft propeller system is responsible for maintaining a selected engine speed power within the propeller. This means that it adjusts the pitch of the propeller blades to maintain a constant speed and prevent overspeeding or underspeeding of the engine. By controlling the propeller speed, the CSU ensures efficient engine operation and optimal performance of the aircraft.

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3. One of the purposes of gudgeon pins in a piston engine is to?

Explanation

Gudgeon pins, also known as wrist pins, play a crucial role in attaching the pistons to their connecting rods in a piston engine. These pins go through the small end of the connecting rod and the piston, allowing them to move in unison. The gudgeon pins provide a pivot point for the connecting rod, allowing it to transfer the reciprocating motion of the piston to the rotational motion of the crankshaft. This connection is vital for the proper functioning of the engine, as it ensures that the piston and connecting rod work together harmoniously to convert the energy from combustion into mechanical power.

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4. The process whereby airflow over the propeller blades of a failed engine keeps the propeller turning is called?

Explanation

Wind milling refers to the process where the airflow over the propeller blades of a failed engine keeps the propeller turning. This occurs due to the force of the wind pushing against the blades, causing them to rotate. This phenomenon can happen when an engine fails or is shut down, and the aircraft is still in motion. The term "wind milling" accurately describes this process as it involves the propeller blades rotating due to the wind's force.

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5. The purpose of the distributor in a piston aero engine, is to distribute?  

Explanation

The purpose of the distributor in a piston aero engine is to distribute high voltage electrical impulse to all cylinders. This is important because it ensures that each cylinder receives the necessary spark at the correct time to ignite the fuel-air mixture and generate power. The distributor acts as a central hub, receiving electrical current from the ignition system and then distributing it to each spark plug in the cylinders. This ensures that the engine runs smoothly and efficiently.

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6. The Blade Twist in the Propeller helps?

Explanation

The blade twist in the propeller helps to even out the thrust along the length of the blade. This is important because it ensures that the propeller generates a consistent amount of thrust throughout its rotation, resulting in smoother and more efficient propulsion. By distributing the thrust evenly, the propeller can maintain a balanced and stable performance, which is crucial for aircraft and other vehicles that rely on propellers for propulsion.

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7. After-burning process in a jet engine requires combustion of additional fuel in the?  

Explanation

The after-burning process in a jet engine requires the combustion of additional fuel in the jet pipe. The jet pipe is a part of the engine that is located after the combustion chamber. It is responsible for directing the exhaust gases out of the engine and creating thrust. By injecting additional fuel into the jet pipe and igniting it, the after-burning process increases the temperature and velocity of the exhaust gases, resulting in a boost in thrust and overall engine performance.

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8. The largest obtainable pitch angle on a variable pitch propeller is referred to as?

Explanation

The largest obtainable pitch angle on a variable pitch propeller is referred to as "Coarse Pitch." This term is used to describe the propeller blades being set at a larger angle, which allows for increased thrust and power during takeoff or when the engine needs to operate at high RPM. The coarse pitch setting helps to generate more lift and acceleration, making it suitable for situations where maximum performance is required.

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9. The two main major of cooling piston aero engines are liquid cooling and air cooling. Which of the following is a major advantage of air cooling over liquid cooling?

Explanation

Air cooling is a major advantage over liquid cooling because it is cheaper to produce. This means that the cost of manufacturing an air-cooled piston aero engine is lower compared to a liquid-cooled engine. This cost advantage can make air-cooled engines more accessible and affordable for manufacturers and customers alike.

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10. Which of these is a turbojet engine?

Explanation

The Olympus 593 is a turbojet engine.

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What is the Major purpose of the fins which are placed around the...
The basic function of the constant speed unit (CSU) in an aircraft...
One of the purposes of gudgeon pins in a piston engine is to?
The process whereby airflow over the propeller blades of a failed...
The purpose of the distributor in a piston aero engine, is to...
The Blade Twist in the Propeller helps?
After-burning process in a jet engine requires combustion of...
The largest obtainable pitch angle on a variable pitch propeller is...
The two main major of cooling piston aero engines are liquid cooling...
Which of these is a turbojet engine?
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