Infrared low-temperature combustion device and method for dual-mass combined cycle turbine
A combined cycle, low-temperature combustion technology, applied in combustion methods, combustion chambers, combustion equipment, etc., to achieve the effects of low manufacturing cost, elimination of thermal damage, and high thermal efficiency
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[0018] see figure 1 , 2 , the names of parts are as follows: Turbine and shaft 1, compressor impeller 2, compressor blade 3, compressor housing 4, lubricating oil inlet 5, fuel inlet 6, infrared grill 7, oil and water nozzle middle body 8, spray Oil nozzle 9, exhaust port 10, water nozzle 11, water nozzle gland 12, annular combustion chamber 13, longitudinal corrugated isolation plate 14, combustion inner wall 15, swirl guide plate 16, turbine blade 17, stator guide plate 18, Invisible heat exchanger 19, warm water outlet 20, exhaust pipe 21, slow decay filling core 22, fuel oil backup inlet 23, second working medium inlet 24, phase change outer wall 25, cold water inlet 26, phase change chamber 27.
[0019] The dual working medium combined cycle turbine includes a moving part, a fuel supply system, a second working medium supply system, an electrical system, a lubrication system, and a load. The specific experimental structure is: it includes a turbine and shaft 1, a right...
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