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Aviation
ch. 10 cooling systems oral questions
14
Aviation
Undergraduate 1
02/09/2014

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Term
what effect does excessive heat have on reciprocating engines
Definition
shortens life of engine parts,
changes behavior of combustion, and
impairs lubrication
Term
what is the purpose of cooling fans
Definition
provide a larger cooling surface area for removing heat from cylinder heads of air-cooled recip engines
Term
what are the reasons for using engine cowlings, baffles and cowl air seals
Definition
reduces drag, and
helps direct airflow over cylinders for cooling
Term
what is the purpose of cowl flaps and how are they operated
Definition
control the amount of airflow through the cowling, they are mechanically, electrically or hydraulically operated
Term
how does an augmenter cooling system work
Definition
an outer tube placed over the exiting exhaust gas creates a venturi effect that draws more airflow over the engine
Term
where should cowl flaps be positioned for ground operations
Definition
fully open
Term
what type of power is used to operate cowl flaps
Definition
manual
hydraulic or
electrical
Term
what should be done when cooling fin damage is discovered
Definition
depending on the damage some cooling fins can be repaired or in extreme cases the cylinder should be replaced
Term
why is cowl flap adjustment important
Definition
the movement must be within tolerances to keep cylinder head temp. within allowable limits
Term
how are turbine engines cooled
Definition
by air passing through the engine
75% cooling
25% combustion
Term
in a turbine engine, where does bleed air come from that is used to cool bearings and other parts
Definition
engine compressor
Term
what is the relationship between turbine engine upper temp. limits and power produced
Definition
the higher the combustion temp. the more power it is capable of producing
Term
what is the approximate % of air passing through a turbine engine that is used for cooling rather than combustion
Definition
75%
Term
what can be done to effectively allow higher gas temp. in the turbine section of some engines
Definition
compressor bleed air ducted through hollow sections in the turbine inlet guide vanes and first stage rotor blades can lower temp. enough to prevent heat damage
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