发明名称 AIRFOIL TRAILING EDGE
摘要 An aerofoil wing comprising upper and lower surfaces meeting at the leading and trailing edges and a camber line representing the curvature of the aerofoil comprising at least two regions of substantially linear increases in curvature and wherein the increases in curvature are of monotonically increasing magnitude. Preferably there are three regions of substantially linear increases in curvature.
申请公布号 WO0038984(A1) 申请公布日期 2000.07.06
申请号 WO1999GB03434 申请日期 1999.10.15
申请人 THE SECRETARY OF STATE FOR DEFENCE;HACKETT, KEVIN, CHRISTOPHER;ASHILL, PATRICK, RALPH;GREEN, JOHN, EDWARD 发明人 HACKETT, KEVIN, CHRISTOPHER;ASHILL, PATRICK, RALPH;GREEN, JOHN, EDWARD
分类号 B64C3/14;(IPC1-7):B64C3/14 主分类号 B64C3/14
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