Invention Application
- Patent Title: High lift longitudinal axis control system
- Patent Title (中): 高升力纵轴控制系统
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Application No.: US12075718Application Date: 2008-03-13
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Publication No.: US20090001225A1Publication Date: 2009-01-01
- Inventor: John Libby
- Applicant: John Libby
- Main IPC: B64C3/14
- IPC: B64C3/14 ; B64C3/38

Abstract:
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. The outboard flap portion is adapted to translate between a first and a second position to create a functional slot between a bottom surface of the flap member leading part and a bottom surface of the airfoil trailing part to draw a portion of higher pressure air from the bottom surface of the airfoil through the functional slot to distribute the higher pressure air over a top surface of the outboard flap portion.
Public/Granted literature
- US07661630B2 High lift longitudinal axis control system Public/Granted day:2010-02-16
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