Engine Cooling Systems Flashcards
The primary purpose of baffles and deflectors installed around cylinders of air-cooled aircraft engines is to what?
force cooling air into close contact with all parts of the cylinders.
What is the purpose of an augmenter used in some reciprocating engine exhaust systems?
To aid in cooling the engine.
Aircraft reciprocating engine cylinder baffles and deflectors should be repaired as required to prevent loss of what?
cooling.
Which of the following should a mechanic consult to determine the maximum amount of cylinder cooling fin that could be removed when cracks are found?
Engine manufacturer’s service or overhaul manual.
Cracks in cooling fins that do not extend into the cylinder head…
may be repaired by removing the affected area and contour filing within limits.
A bent cooling fin on an aluminum cylinder head should be what?
left alone if no crack has formed.
Where are cooling fins usually located on air-cooled engines?
Cylinder head, cylinder barrel, and inside the piston.
How do cowl flaps aid in cooling a horizontally opposed aircraft engine?
Controls the amount of air flowing around the cylinders.
The position of the cowl flaps during normal cruise flight conditions is what?
closed.
Generally, a small crack just started in a cylinder baffle…
may be stop drilled.
Which of the following assists in removing heat from the metal walls and fins of an air-cooled cylinder assembly?
A baffle and cowl arrangement.
During ground operation of an engine, the cowl flaps should be in what position?
Fully open.
The component(s) in a turbine engine that operate(s) at the highest temperatures is/are the what?
first stage turbine nozzle guide vanes.
During an operational check of an electrically powered aircraft engine cowl flaps system, the motor fails to operate. Which of the following is the first to be checked?
Flap actuator motor circuit breaker.
(1) Some aircraft exhaust systems include an augmenter system to draw additional air over the engine for cooling.
(2) Augmenter systems are used to create a low pressure area at the lower rear of the aircraft engine cowling.
Both 1 and 2 are true.