发明公开
EP3052812A1 COMPRESSOR AREA SPLITS FOR GEARED TURBOFAN 审中-公开
压缩过程庭的齿轮涡轮风扇

COMPRESSOR AREA SPLITS FOR GEARED TURBOFAN
摘要:
A gas turbine engine has an upstream compressor having an upstream entrance area leading into a first vane upstream of the upstream compressor. A downstream compressor has an exit area at a leading edge of an exit vane for the downstream compressor. The entrance area divided by the exit area is greater than or equal to 13.8 and less than or equal to 15.3.
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