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
2024-04-10
Patent
Electronic Resource
English
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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