发明名称 NESTED CORE GAS TURBINE ENGINE
摘要 A fan for creating lift or thrust having a fan hub and fan blades depending from the fan hub. The fan blades have slots formed therein with openings facing substantially aft, relative to a rotation direction of the fan blades, wherein air blowing from the fan hub into the fan blades and out of the openings of the slots contribute to the aerodynamic performance of the fan blades to enhance the aerodynamic performance of the fan blades.
申请公布号 US2010034640(A1) 申请公布日期 2010.02.11
申请号 US20090537046 申请日期 2009.08.06
申请人 DEV SUDARSHAN PAUL 发明人 DEV SUDARSHAN PAUL
分类号 F01D5/14;F02C3/045;F02C3/06;F02C3/067;F02C3/10;F02C3/16;F02C7/10;F02K3/068 主分类号 F01D5/14
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