Gas turbine inlet double-loop cooling system and method utilizing refrigerating station cooling capacity allowance
A gas turbine and cooling system technology, which is applied to gas turbine installations, engine cooling, turbine/propulsion cooling, etc., and can solve the impact of peak shaving capacity and unit performance, reduction of combined cycle unit output and thermal efficiency, and increase in gas turbine inlet temperature. Advanced problems, to achieve the effect of low investment cost, realize operation, improve output and thermal efficiency
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[0025] In order to make the purpose and technical solution of the present invention clearer and easier to understand. The present invention will be further described in detail below in conjunction with the drawings and embodiments. The specific embodiments described here are only used to explain the present invention, not to limit the present invention.
[0026] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", " The orientations or positional relationships indicated by "vertical", "horizontal", "top", "bottom", "inner" and "outer" are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and Simplified descriptions, rather than indicating or implying that the device or element referred to must have a particular orientation, be constructed and operate in a particular ori...
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