发明名称 Gas turbine blade cooling arrangement
摘要 <p>In order to couple coolant air flow presented through a coolant gallery 4, 24 through an opening 7, 27 into a passage 8, 28 a flow deflector 6, 26 is provided. The flow deflector 6, 26 progressively deflects the coolant air flow 5, 25 through the opening 7, 27 such that there is reduced loss in coolant flow 5, 25 pressure.</p>
申请公布号 EP1424468(A3) 申请公布日期 2006.05.10
申请号 EP20030257022 申请日期 2003.11.06
申请人 ROLLS-ROYCE PLC 发明人 TOWNES, RODERICK MILES
分类号 F01D5/18;F01D5/08 主分类号 F01D5/18
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