发明名称 |
Gas turbine engine modular cooling and heating apparatus |
摘要 |
The present invention comprises a modular unit in which all of the components necessary for conditioning the intake air for a combustion gas turbine are contained. The compressors, evaporators condensers and related pumps and control equipment are contained within a weather proof enclosure having sound insulation installed in the walls. The intake air conditioning system includes three loops, a compressed refrigerant loop, a chilled water loop and a condenser cooling water loop with an optional heating loop. The modular unit provides a three loop cooling system for easy connection to both a combustion gas turbine air inlet and to a cooling water tower. The loops comprise a refrigerant loop, a cooling water loop and a chilled water loop and in one embodiment a heating loop to heat the air going to the turbine.
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申请公布号 |
US6422018(B1) |
申请公布日期 |
2002.07.23 |
申请号 |
US20000640836 |
申请日期 |
2000.08.17 |
申请人 |
TISDALE LLOYD B.;HAUCK ROBERT L.;TISDALE, JR. PAUL T. |
发明人 |
TISDALE LLOYD B.;HAUCK ROBERT L.;TISDALE, JR. PAUL T. |
分类号 |
F02C7/04;F02C7/143;(IPC1-7):F02C7/143 |
主分类号 |
F02C7/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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