Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1997-10-20
2000-11-28
Poon, Peter M.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244 35R, 244212, B64C 344
Patent
active
061524050
ABSTRACT:
A lift body has a variable camber to achieve a flow-favorable profile. The lift body has a structure which is elastically deformable at least in one area. An integrated adjusting device includes at least one dimensionally stable adjusting body which can be rotated about an axis and which is in an operative connection with the deformable structure. Each adjusting body has a curved conical shape whose local cross-section corresponds to the local profile thickness. Each adjusting body is in a direct and/or, via a sliding layer, an indirect contact with the deformable structure.
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Daimler-Benz Aerospace AG
Dinh Tien
Poon Peter M.
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