How do the high-velocity high-temperature gases cause the gas turbine rotor to rotate?
β’ Energy conversion in a gas turbine β how kinetic (velocity) and thermal (heat) energy of the gas interact with turbine blades β’ Action of gas on turbine blades β how the shape of blades turns straight gas flow into rotational motion β’ Difference between velocity increase/decrease and energy transfer to the rotor
β’ When hot, fast-moving gas strikes turbine blades, what happens to the gasβs speed and direction, and where does that energy go? β’ Which choice best describes energy being taken from the gas and given to the rotor, rather than just changing the gasβs speed for its own sake? β’ In a working turbine, does the gas leave the turbine with more or less energy than it entered with, and what does that imply about the rotor?
β’ Identify which option talks about energy being passed from the gas to the blades/rotor, not just changing gas conditions by themselves. β’ Ask: in a turbine, is rotation produced mainly by creating a low-pressure area ahead of the rotor or by the gas doing work on the blades? β’ Check whether the option you pick would result in the gas losing energy while the rotor gains mechanical energy.
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