DESIGN AND ANALYSIS OF A BIOFUEL-POWERED MICRO GAS TURBINE COMBUSTION CHAMBER
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Abstract
Small combustion turbines known as micro turbines provide power in the 20 kW to 500 kW
range. Small jet engines, auxiliary power units (APUs) for aircraft, and turbochargers for cars
and trucks are the origin of the Evolution. A relatively recent development in distributed
generation, micro turbines are employed in stationary energy generation applications. In most
cases, they are combustion turbines, which on a small scale generate heat as well as power.
Radial inflow turbine, combustor, and centrifugal compressor are the three main components
of a micro (gas) turbine engine. Along with turning the compressor, it also serves as a power
output. For distributed electricity and cogeneration (combined heat and power) applications,
micro turbines are becoming more and more common. The micro turbine and gas turbine cycles
both run continuously. Studying a brief description of SOLIDWORKS modelling is necessary.
With the aid of Solid works, several turbine components (includes the housing, connection,
exit, rotor, nozzle, storage, inlet, and so on) are designed (software). They were then put
together as one unit and attached to a generator to produce electricity. The axial intake and
axial output of the turbine indicate its kind.
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