A turbo is a type of combustion, often to drive the machinery. The air compressor is used in the rotary switch on the intake of water and compressed to a higher before entering the combustion chamber. The fuel is supplied with the compressed air and ignited a small flame in the vortex of a flame holder.
This increases the combustion temperature of the gas. Combustion heat from the combustion of chemicals by the expansion of the turbine, where the power is the use of the compressor. Although this expansion process reduces the temperature and pressure of gas from the turbine, the two variable are in most cases significantly above the ambient. The gas flow from the turbine to the ambient pressure increases by the jet propulsion systems, leading to a beam with high velocity in exhaust Panache. So, if the power from the speed of the flight speed, it creates a push forward.
Under normal circumstances, the pumping action of the compressor prevents reflux, we can also load on the engine to respond. You can find the whole process with a cycle of four, but with the induction, spark-ignition engine, the growth and the exhaust system, which at the same time. The effectiveness of a jet engine is strongly dependent on the ratio (input combustion pressure / decrease of pressure) and the turbine inlet temperature of the cycle.
Perhaps it is also instructive to compare jet engine propeller engines. Turbo, a small mass of air and the acceleration of a large quantity, when the propeller has a variety of air and accelerates it a small amount.
In high velocity of the exhaust of an engine to respond, the efficiency at high speeds (especially supersonic speed) and at high altitude.
On airplanes, which fly slow and low range, a gas turbine, caused by the propeller of the engine, commonly known as a turboprop, much more frequently and more efficiently. Especially small conventional engines used primarily for the operation of a screw, but small turboprops are getting smaller as the technology improves every day.
The Turbo is the top one role of design, where a tree connects the turbine of the compressor pressure ratio is higher models are often associated with two concentric shafts, it is fundamentally aimed at improving the stability of the compressor motor in moving gas.
In general, it is outside the bar, the high pressure turbine rotor components of the compressor. The combustion chamber with high pressure compressor is the core of the coil or generator-gas engine. We must not forget that the inside of the shaft connects the low pressure compressor to the LP turbine to the LP Spool. Each of the rollers are free to operate their optimal tree.