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经营范围
发明名称
High lift longitudinal axis control system
摘要
A bipartite, full span airplane flap system having an inboard flap portion and an outboard flap portion, wherein the outboard flap portion includes an integrated aileron mounted on its substantially equivalent spanwise length.
申请公布号
US2006169848(A1)
申请公布日期
2006.08.03
申请号
US20050047194
申请日期
2005.01.31
申请人
LIBBY JOHN
发明人
LIBBY JOHN
分类号
B64C9/16
主分类号
B64C9/16
代理机构
代理人
主权项
地址
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