| 发明名称 | Turbine inlet air heat pump-type system | ||
| 摘要 | A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a thermal energy storage tank charging loop, a cooling loop in communication with the thermal energy storage charging loop, and a heating loop in communication with the cooling loop and the inlet air of the turbine compressor. | ||
| 申请公布号 | US9470149(B2) | 申请公布日期 | 2016.10.18 |
| 申请号 | US200812332383 | 申请日期 | 2008.12.11 |
| 申请人 | General Electric Company | 发明人 | Motakef Abbas;Feher Peter |
| 分类号 | F02C7/143;F01K27/02;F02C7/047;F01K23/10 | 主分类号 | F02C7/143 |
| 代理机构 | Sutherland Asbill & Brennan LLP | 代理人 | Sutherland Asbill & Brennan LLP |
| 主权项 | 1. A heating and cooling system for inlet air of a gas turbine compressor, comprising: one or more water chillers comprising an evaporator and a condenser; a thermal energy storage tank charging loop comprising the evaporator of the one or more water chillers; a cooling loop comprising the condenser of the one or more water chillers, wherein the cooling loop is in communication with the thermal energy storage tank charging loop via the one or more water chillers; and a heating loop in communication with the cooling loop via a heat exchanger such that waste heat from the condenser of the one or more water chillers is exchanged in the heat exchanger to the heat loop, wherein the heating loop is in communication with the inlet air of the turbine compressor. | ||
| 地址 | Schenectady NY US | ||