A stamping intercooled gas turbine
A technology of gas turbine and compressor casing, which is applied in the direction of gas turbine devices, mechanical equipment, engine components, etc.
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[0020] A rammed intercooled gas turbine, including a compressor casing, multi-stage compression, RSS steady-flow burner, turbofan casing, and multi-stage turbofan, divided into four parts that are connected end to end, and each part is based on the same straight line as the axis ,bilateral symmetry;
[0021] The first part is composed of the first stage compressor shell, the first group of multi-stage compression, the first stamping tube, and the second stamping tube; the first group of multi-stage compression is located in the first stage compressor shell, and more than 2 stamping tubes Distributed outside the compressor casing of the first stage; the front end of the multi-stage compression is connected to the air to be compressed, the front end of the first stamping tube and the second stamping tube are connected to the cold air, and the rear end of the multi-stage compression is connected to the first stamping tube The rear ends of the tube and the second stamping tube are...
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