Gas Turbine Generator Drawing

The rotation of the shaft drives the compressor to draw in and compress more air to sustain continuous combustion.

Gas turbine generator drawing. For example the end of the isentropic compression performed by the compressor is designated with a 3 on a t s diagram. Approximately 55 to 65 percent of the power produced by the turbine is used to drive the compressor. The brayton cycle describes the thermodynamics of a gas turbine engine and when describing the processes on a p v or t s diagram we denote the end of a process by using the station number. Beyond the turbine end of the gas generator is a freely rotating turbine.

Each step deals with an aspect of the project and a suggested design. Compressorair compressor used in a gas turbine power plant is mainly of the rotary type. The air filter is attached at the inlet of the compressor where air gets. The compressor which draws air into the engine pressurizes it and feeds it to the combustion chamber at speeds of hundreds of miles per hour.

Diy gas turbine 5 steps. It is not mechanically connected to the gas generator but instead is mechanically coupled 1 1 gas turbines in simple cycle and combined cycle applications. The combustion gas turbines being installed in many of today s natural gas fueled power plants are complex machines but they basically involve three main sections. Ge s advanced gas path agp is a great example of power flexefficiency at work setting new standards in performance.

The remaining shaft power is used to drive a generator which produces electricity. It may be one or more stages. I do not recommend anybody to try any of this but if you are going to try it this is the way you should do it this instructable deals with how to build a gas turbine in 5 steps. The main components of a gas turbine power plant are the compressor regenerator combustion chamber gas turbine alternator and starting motor.

A gas turbine also called a combustion turbine is a type of continuous and internal combustion engine the main elements common to all gas turbine engines are. A fourth component is often used to increase efficiency on turboprops and turbofans to convert power into mechanical or. An upstream rotating gas compressor.