engine cooling systems Flashcards

1
Q

what are the three main reasons that excessive heat is undesirable in any reciprocating engine

A
  1. it affects the behavior of combustion
  2. it weakens and shortens the life of engine parts
  3. it impairs lubrication
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2
Q

what is used to provide sufficient cooling surface area for air cooled reciprocation engines

A

cooling fins

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3
Q

what happens to waste engine heat after it is transferred to cylinder cooling fins

A

it is further transferred from the engine cylinders to the air

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4
Q

what should be done to a cylinder with excessive cooling fin area broken off

A

replace the cylinder

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5
Q

what is the principle function of engine cowling and baffles

A

to direct airflow over the cylinders for cooling

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6
Q

what is used to control the amount of airflow through the cooling area of a reciprocating engine

A

cowl flaps

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7
Q

what is an augmentor cooling system

A

it is an exhaust system incorporating inner and outer tubes that uses exiting exhaust gas velocity to produce a venturi effect to draw more airflow over the engine

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8
Q

what type power is used to operate cowl flaps

A

manual, electrical, hydraulic

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9
Q

why do some aircraft use augmentors

A

to provide additional cooling airflow

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10
Q

where should cowl flaps be positioned during ground operations

A

fully open

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11
Q

what information must be consulted prior to re-profiling a cooling fin

A

the manufacturer’s maintenance manual

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12
Q

what are the functions of engine cowling

A

it streamlines the engine area to reduce drag, and it forms an envelope around the engine to aid in controlling airflow

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13
Q

what is the purpose of cowl seals

A

they force air to circulate around and through the baffle system

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14
Q

why is cowl flap adjustment important

A

the movement must be within tolerances to keep cylinder head temperatures within allowable limits

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15
Q

where must most cooling airflow to cool a turbine engine

A

through the inside of the engine

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16
Q

what areas of a turbine engine are cooled by air passing through the engine

A

the combustion chamber and turbine

17
Q

what is the source of bleed air vented to turbine engine bearings and other parts in some engines

A

the engine compressor

18
Q

what is the approximate percentage of air passing through a turbine engine that is used for cooling rather than combustion

A

75%

19
Q

what is the relationship between turbine engine and upper temperature limits and power produced

A

the higher the combustion temperatures that an engine can withstand without damage, the more power it is capable of producing

20
Q

how is compressor bleed air used to effectively allow higher gas temperatures in the turbine section of some engines

A

bleed air from the compressor is ducted through hollow turbine section inlet guide vanes and hollow first stage rotor blades, keeping them cool enough to prevent damage