Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1983-09-30
1987-02-10
Basinger, Sherman D.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244123, B64C 314
Patent
active
046417966
ABSTRACT:
An airfoil member having an upper surface contoured to create lift. The lower airfoil surface has a lower forward surface portion which, in a rearward direction, curves concavely into an expanded convexly curved lower surface belly portion. This enables a primary load carrying member (e.g. a spar) to be located in the belly section and have a relatively greater depth, without unnecesary sacrifice of aerodynamic performance. In another embodiment, both the upper and lower surfaces of the airfoil are contoured with the expanded belly portion.
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Basinger Sherman D.
Corl Rodney
The Boeing Company
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