发明名称 Air bypass system for gas turbine inlet filter housing, surrounds internal cooling system increasing performance and includes butterfly valve for throttling
摘要 <p>The air bypass system (110) of a gas turbine inlet filter housing (100) includes an internal system increasing performance (40), especially a cooler. A channel (120) passes around the system (40), on the inlet filter housing (100). It contains a butterfly valve for throttling by opening and closing the channel. Further side- (120, 130) and upper- (140) channels are included. The channel (120) includes polymer. In use, the area for airflow is increased through the system, which is brought into action. The air flow area is then reduced during operation. An independent claim is included for the corresponding method of operation.</p>
申请公布号 DE102007028583(A1) 申请公布日期 2007.12.27
申请号 DE20071028583 申请日期 2007.06.19
申请人 GENERAL ELECTRIC CO. 发明人 SMITH, RAUB WARFIELD;CHILLAR, RAHUL J.;SCIPIO, ALSTON ILFORD
分类号 F02C7/057 主分类号 F02C7/057
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