due to diposition over blade HEAT
There has to be a built in expansion chamber or release valve. Otherwise the expansion would cause an explosion.
Scoop coupling is nothing but a fluid coupling works based on the hydro dynamic principle. Scooping is the collecting the oil from the working chamber(space between pump wheel and turbine wheel) which will effects the transmission.
It sends hot gases from the combustion chamber to the 1st stage turbine blades at the correct angle and speed
Some varieties of gas turbine engines (e.g. RR Trent and RB211) have 3 concentric rotating shafts. Each shaft connects a compressor with a turbine. The low pressure compressor, or fan, is driven by the low pressure turbine. The high pressure compressor is driven by the high pressure turbine. Between the low and high pressure compressors there is an intermediate pressure compressor and, guess what... it's driven by the intermediate pressure turbine.
due to diposition over blade HEAT
Essentially its the pressure prior to entering the turbine chamber via the MSV (main stop valve)
Do not read this answer or Weegee will get you!
Short for turbocharger, It is an exhaust driven air compressor. Exhaust gases exit the engine and enter the turbine housing where it spins the turbine wheel. The turbine wheel is connected to a shaft which the compressor wheel is also attached. When more power is needed, the turbine/compressor wheel assembly spins faster and the compressor wheel sucks in more air and compresses it creating boost/positive manifold pressure/more power.
mix-pressure turbine
There has to be a built in expansion chamber or release valve. Otherwise the expansion would cause an explosion.
Basically, a gas turbine is powered by gas under pressure, The gas is pressurized by burning some type of fuel such as kerosene, jet fuel, or propane. That heat causes air expansion, and the subsequent inflow of air makes the turbine spin. A gas turbine consists of three main parts; a combustion chamber, a turbine and a compressor. Air and fuel are mixed in the combustion chamber where it is ignited and increases in speed and power. This power is directed over the turbine blades which spin the turbine and power the compressor. It's a pretty simple process: heated fuel causes pressure and air expansion. The expanded air causes a turbine to spin. That is how gas turbines like jet engines work.
Scoop coupling is nothing but a fluid coupling works based on the hydro dynamic principle. Scooping is the collecting the oil from the working chamber(space between pump wheel and turbine wheel) which will effects the transmission.
It sends hot gases from the combustion chamber to the 1st stage turbine blades at the correct angle and speed
Some varieties of gas turbine engines (e.g. RR Trent and RB211) have 3 concentric rotating shafts. Each shaft connects a compressor with a turbine. The low pressure compressor, or fan, is driven by the low pressure turbine. The high pressure compressor is driven by the high pressure turbine. Between the low and high pressure compressors there is an intermediate pressure compressor and, guess what... it's driven by the intermediate pressure turbine.
A turbine or water wheel,
a turbine would be used instead of a water wheel because a turbine does not use as much energy and it uses the wind to generate it.