In some examples, a wing for an aircraft, the wing having a passive variable aeroelastic geometry for accommodating efficient flight at multiple aircraft speeds, comprises a wing skin comprising a composite structure comprising a lamination of multiple layers deposited for the wing skin according to a predetermined lamination profile, at least one of the layers comprising a continuous non-linear deposition of material, the wing skin comprising a stiffness distribution profile defined by the lamination profile.
AIRCRAFT WINGS COMPRISING AN AEROELASTICALLY TAILORED COMPOSITE STRUCTURE
FLUGZEUGFLÜGEL MIT AEROELASTISCH ANGEPASSTER FASERVERBUNDSTRUKTUR
AILES D'AVION COMPRENANT UNE STRUCTURE COMPOSITE AEROELASTIQUEMENT CONFECTIONNÉE
10.04.2024
Patent
Elektronische Ressource
Englisch
IPC: | B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B29D PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE , Herstellen besonderer Gegenstände aus Kunststoff oder aus Stoffen in plastischem Zustand / B64C AEROPLANES , Flugzeuge / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung |
Aeroelastically Tailored Propellers
SAE Technical Papers | 1977
|Aeroelastically tailored wing design
AIAA | 1980
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