发明名称 IMPROVED SLAT CONFIGURATION FOR FIXED-WING AIRCRAFT
摘要 A slat for fixed-wing aircraft that includes a leading edge, a trailing edge, a chord, and an inboard edge that includes particular dimensions to affect airflow over the wing.
申请公布号 US2011049305(A1) 申请公布日期 2011.03.03
申请号 US20080866679 申请日期 2008.02.12
申请人 BOMBARDIER INC. 发明人 KAFYEKE FASSI;LANGLOIS MARC;KHO CEDRIC
分类号 B64C9/24 主分类号 B64C9/24
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