发明名称 Fan for a gas turbine engine air intake
摘要 A ducted fan gas turbine engine spinner is so configured so as to be generally outwardly flared at its downstream end. The flared portion provides a decrease in the local axial velocity of the air flow over the spinner. This in turn leads to the reduction or elimination of choking in the radially inner region of the fan of the engine.
申请公布号 US5224833(A) 申请公布日期 1993.07.06
申请号 US19920921971 申请日期 1992.08.04
申请人 ROLLS-ROYCE PLC 发明人 NICHOLAS, DAVID J.;MORTIMER, TONY F.
分类号 B64C11/14;F02C7/04 主分类号 B64C11/14
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