A tail sitter aircraft (1', 1 ") is described, comprising a wing (4) with a closed front section (C); a fuselage (2), from which said wing extends; said fuselage extending parallel to a first axis (Y); said wing being a non-planar wing closed in on itself and without free ends; said wing comprising a first portion (5) projecting from said fuselage, a second portion (6) spaced from said first portion; and - a first and a second connecting section (7), which are interposed between respective ends (8, 9) of said first portion (5) and of said second portion, said first portion and said second portion being parallel to one another and extending parallel to a second axis (X) orthogonal to said first axis (Y), said first axis (Y) being arranged, in use, vertically in a take-off/landing position and inclined with respect to the vertical direction in a cruising position. Said first and a second connecting section extend parallel to a third axis (Z) orthogonal to said second axis and to said first axis, said wing comprising a third portion (30) arranged on the opposite side of said first portion with respect to said second portion and connected to said first portion at their respective ends (32, 8) by first sections (31) extending parallel to said third axis.

    L'invention concerne un aéronef à décollage et atterrissage verticaux (1, 1', 1'', 1''', 1''''') comprenant une aile (4) possédant une section avant fermée (C).


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    Title :

    TAIL SITTER


    Additional title:

    AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX


    Contributors:

    Publication date :

    2020-02-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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