The major function of the turbine in the turbojet is that it supplies the power to turn the compressor. An automatic fuel control unit on a turbojet engine is influenced by the burner pressure.
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They do not have moving parts (e.g. compressor blades, shaft, turbine blades) needed by turbojet engines, increasing reliability, reducing maintenance costs, and permitting them to operate at faster airspeeds. However neither can be used at low airspeeds at all, being a significant disadvantage as a different engine (e.g. turbojet, rocket) must also be provided for takeoff and landing.
by controlling main steam flow
Essentially its the pressure prior to entering the turbine chamber via the MSV (main stop valve)
The main parts are the tower, the generator, the blades, the pitch regulator, the inverter and the maintenance men.
The difference is that geysers are way much hotter than the steam from hot springs. The geysers can give you 3rd degree burns. But so can the steam from hot springs if you're in there to long.