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www.TURBIVO.com The variable VOlume TURBIne finally within your grasp |
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Background General principlesThermodynamics: - laws - transformations - operation - classification - cycles - requirements - combustion - performance Mechanical configuration: - petrol engines - gas oil engines - gas turbines Concerns: - lubrification - cooling - exhaust fumes Summary and conclusion |
2 - Background2.2 - Specific examples2.2.2 - Mechanical design of heat engines2.2.2.4 - LubrificationThe most widely used engine has the most complex lubrication system. This is because the reciprocating engine has many lubrication points, in particular the piston-compression rings-cylinder assembly or cylinder sleeve which is the most difficult to lubricate for two reasons:
In this respect, the gas turbine is more practical since the blades do not come into contact with their respective housing. 2.2.2.5 - CoolingGiven the fact that burning oils lose their power to lubricate, and the configuration of the the reciprocating engine, then the parts that are exposed to the heat generated by combustion must undergo intensive cooling to prevent the oil from losing its lubricating capacity. This cooling causes the forced evacuation of over 30% of the thermal energy in the fuel, thereby removing part of the input heat.. 2.2.2.6 - Exhaust fumesIn reciprocating engines over 30% of the energy in the fuel is dissipated through the exhaust:
In gas turbines, the time lags for the combustion gases to pass through are too short to allow expansion and cooling to occur which would limit exhaust losses. It follows that 70 to 80% of the thermal energy in the fuel is dissipated in the form of heat, except where this heat is partially transmitted to the compressed air through a heat exchanger. ****** |
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