发明名称 |
Method of heating gas turbine inlet |
摘要 |
<p>METHOD OF HEATING GAS TURBINE INLET An air inlet system delivers a flow of air. The system included a temperature controlling section configured to alter temperature of the air flow. The temperature controlling section imparts a temperature variation distribution across different portions of the air flow. The system also includes a transition section, one or more flow diverters, one or more screens and/or a flow splitter to cause mixing of the different, temperature variant portions of the air flow and reduce the temperature variation distribution. Fig. 2</p> |
申请公布号 |
AU2012232951(A1) |
申请公布日期 |
2013.05.02 |
申请号 |
AU20120232951 |
申请日期 |
2012.09.28 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
RAJESH, PRABHAKARAN SARASWATHI;CHILLAR, RAHUL JAIKARAN;KIPPEL, BRADLEY AARON;CONRAD, RICKY DARYL |
分类号 |
F02C7/04;F02C7/042 |
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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