Edge morphing arrangement for an airfoil

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Edge morphing arrangement for an airfoil

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KOTA SRIDHAR / ERVIN GREGORY F / LO JIA-HSUAN / LU KERR-JIA / MARIC DRAGAN / TROST MARK R / TSANG RUEY-KHAN K

An edge-morphing arrangement for an airfoil includes a compliant upper surface and a compliant lower surface that are joined together. An actuator is coupled to a driven surface and actuated to move the driven surface and change the shape thereof, with the non-driven surface changing its shape in response to actuation of the driven surface. The upper and lower surfaces can be part of a sub-flap mounted to a traditional flap of the fixed wing of an airplane. The upper and lower surfaces can be mounted to existing structure in the flap, or the flap components can be mounted to the sub-flap. The upper and lower surfaces can alternatively replace the traditional flap in the fixed wing of an aircraft. The upper and lower surfaces are continuous and can be deflected upward, downward, or twisted in a span-wise direction relative to the flap or wing.

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Dokumentinformationen

Titel :

Edge morphing arrangement for an airfoil

Beteiligte:

KOTA SRIDHAR (Autor:in) / ERVIN GREGORY F (Autor:in) / LO JIA-HSUAN (Autor:in) / LU KERR-JIA (Autor:in) / MARIC DRAGAN (Autor:in) / TROST MARK R (Autor:in) / TSANG RUEY-KHAN K (Autor:in)

Erscheinungsdatum :

2018-09-06

Medientyp :

Patent

Format :

Elektronische Ressource

Sprache :

Englisch

Klassifikation :

IPC:

B64C AEROPLANES , Flugzeuge

Edge morphing arrangement for an airfoil

Edge morphing arrangement for an airfoil

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