发明名称 High lift and high strength aerofoil
摘要 A high lift stepped aerofoil section, incorporating a leading edge 1, trailing edge 3 and a step 2 to provide a higher vertical component in its construction; the aerofoil has greater perceived root thickness giving greater lift through compression 4 on the aerofoil under surface. The section has high pressure area 5 below the aerofoil and low pressure area 6 above the aerofoil. The aerofoil has much higher strength on all axes than conventional aerofoil sections.
申请公布号 US2007158495(A1) 申请公布日期 2007.07.12
申请号 US20070717283 申请日期 2007.03.14
申请人 HUBBARD ADRIAN A 发明人 HUBBARD ADRIAN A.
分类号 B64C3/14;B64C11/18;B64C27/467;F04D29/38 主分类号 B64C3/14
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