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External cooling
Cooling of the external skin of an aero-engine is achieved by suitable design of the aircraft airframe; the layout will depend upon where the engine is fitted and what kind of engine compartment is used. Normally, the cooling and ventilating of an engine bay or pod is achieved by ducting atmospheric air round the engine and spilling it back to atmosphere through suitably placed outlets (see figure). The air is usually taken from a ram inlet but provision is also made to provide a cooling and ventilating airflow during ground running periods. Another function of the cooling airflow is to remove flammable vapours from the engine compartment to reduce the fire risk.
numericals
Cold junction compensation A recent solution to the problem of controlling a reference junction temperature is to use a 'cold-junction compensator'. This is an integrated circu
Slipstream Effect. In passing through the propeller the air is accelerated and given a rotational velocity. The parts of the aircraft that are in the propeller slipstream wi
Mechanical pulverization method is applicable to brittle metals like antimony. Many varieties of mechanical pulverizers are in use; some of these have counter rotating plates or r
Electrical ice protection systems: Electrical ice protection systems are used on most turbo-props. Resistance wire heater elements are embedded in rubber and cemented from the
Fire risk assessment process: This is the main part of the FRA process. Here we consider the risk, measure it against what we consider acceptable and, if we consider that t
what is electrical transmission and electromagnetic radiation in the form of energy transfer?
How to I make my archimedes screw work?
Cathode ray tube (crt): Displays of this type, which are based on the electron beam scanning technique, have been used in aircraft for many years. They were first used to disp
Can u provide some information about simple wireless transmitter and receiver.
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