发明名称 ACTIVE CLEARANCE CONTROL SYSTEM FOR A TURBOMACHINE
摘要 <p>An axial compressor is provided with a cooling air manifold surrounding a portion of the shroud, and means for bleeding air from the compressor to the manifold for selectively flowing it in a modulating manner axially along the outer side of the stator/shroud to cool and shrink it during steady-state operating conditions so as to obtain minimum shroud/rotor clearance conditions. Provision is also made to selectively divert the flow of cooling air from the manifold during transient periods of operation so as to alter the thermal growth or shrink rate of the stator/shroud and result in adequate clearance with the compressor rotor.</p>
申请公布号 GB2054741(B) 申请公布日期 1983.10.05
申请号 GB19800024092 申请日期 1980.07.23
申请人 GEC US 发明人
分类号 F04D29/54;F01D11/24;F02C7/28;F04D29/58;(IPC1-7):04D29/58 主分类号 F04D29/54
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