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Gas turbine fuel properties and specificationIn the earliest days of the gas turbine engine, kerosene was regarded as the most suitable fuel. It commended itself on the grounds of availability, cost, calorific value, burning characteristics and low fire hazard.
Other types of petroleum fuels are not suitable for use in gas turbines because of the wide range of temperature and pressure over which combustion must occur and the necessity of keeping the weight and volume to a minimum.
A gas turbine fuel should have the following qualities:a) Ease of flow under all operating conditions.b) Quick starting of the engine.c) Complete combustion under all conditions.d) A high calorific value.e) Non-corrosive.f) The by-products of combustion should have no harmful effect on the flame tubes, turbine blades, etc.g) Minimum fire hazards.h) Provide lubrication of the moving parts of the fuel system. i) The by-products of combustion should have minimal harmful effect on the environment
Reduction Gearing : Compound epicyclic reduction gears enable a greater reduction in speed to be obtained without resorting to larger components. They may be of either the fix
1 Scott Investors, Inc., is considering the purchase of a $447,000 computer with an economic life of five years. The computer will be fully depreciated over five years using the st
Couplings: Because of the requirement to make maintenance tasks such as engine removal/refit, gearbox removal/refit easier, it is necessary to have a means of coupling the turb
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Bearing stresses are very common in aerospace engineering. It occurs on the surface of contact between any two structural members. Bolts, pins, and rivets are classic examples of
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