发明名称 Air intake for turboprop engine, especially aircraft engine, has fixed cutting blades inside air duct to chop ingested items into sufficiently small pieces to prevent turbine damage
摘要 An air intake for a turboprop engine, especially aircraft engine, has an intake duct (14) contoured around the transmission (13) and fitted with internal fixed cutting blades which chop any ingested items into sufficiently small pieces which do not damage the turbine. The blades are positioned in any suitable alignment especially across the airflow and in line with the airflow, and on the insides of bends in the duct.
申请公布号 DE102004004980(A1) 申请公布日期 2005.09.01
申请号 DE20041004980 申请日期 2004.01.31
申请人 MTU AERO ENGINES GMBH 发明人 ROSSMANN, AXEL;SIKORSKI, SIEGFRIED
分类号 B64D27/10;B64D33/04 主分类号 B64D27/10
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