An aircraft with a fuselage and with wings connected thereto, wherein a support strut extends between the fuselage and each of the wings, which support strut is connected both to the fuselage and to the wing. The support strut has a hydraulic working cylinder, which can be pressurized with hydraulic fluid in a controlled manner for the purpose of pivoting the wing.
AIRCRAFT HAVING HYDRAULIC SUPPORT STRUTS BETWEEN FUSELAGE AND WINGS
31.08.2017
Patent
Elektronische Ressource
Englisch
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