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    AERONEF A VOILURE FIXE ET A STABILITE STATIQUE ACCRUE
    1.
    发明公开
    AERONEF A VOILURE FIXE ET A STABILITE STATIQUE ACCRUE 审中-公开

    公开(公告)号：EP3365226A1

    公开(公告)日：2018-08-29

    申请号：EP16806217.2

    申请日：2016-10-21

    申请人： Danielson Aircraft Systems

    发明人： HUBSCHWERLEN, Frédéric

    IPC分类号： B64C21/02 ,  B64C23/06 ,  B64C39/06

    摘要： The invention relates to an aircraft having at least one wing (5) including, at each end thereof, a fin (6) forming an angle of between 0° and 45° relative to the vertical. According to the invention, each fin (6) has a leading edge (7) that includes at least one slot (8) provided along said leading edge (7) and oriented so as to cause an air flow to flow via said leading edge (7) from an outer surface (6a) of the fin (6) to an inner surface (6b).

    VEHICULE AERIEN AVEC DES AILES POLYGONALS
    2.
    发明公开
    VEHICULE AERIEN AVEC DES AILES POLYGONALS 有权

    公开(公告)号：EP3154856A1

    公开(公告)日：2017-04-19

    申请号：EP15732849.3

    申请日：2015-06-10

    申请人： Danielson Aircraft Systems

    发明人： HUBSCHWERLEN, Frédéric

    IPC分类号： B64C39/06

    CPC分类号： B64C39/068 ,  B64C1/30 ,  B64C3/16 ,  B64C3/56 ,  B64C9/14 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/102 ,  B64C2201/127

    摘要： An aircraft comprising at least two lateral fuselages (2) connected by a wing (4), at least one propulsion means, and two lateral wings (5) respectively extending from the lateral fuselages (2) and respectively having a front cross-section in the shape of a polygon with at least four sides, characterized in that: - the propulsion means (3) consists of a motor carried by each lateral fuselage (2) and respectively driving a propeller (6), - the ratio between the height of the lateral wings (5) and the wingspan of the aircraft is between 0.15 and 0.25; - each lateral wing (5) consists of a first wing part (5a) extending in the same plane as the wing (4), a second wing part (5b) extending vertically above the first wing part (5a) and being inclined from front to rear and from bottom to top, a third wing part (5c) extending parallel to the first wing part (5a) and extending from front to rear by forming an angle with the front plane of the aircraft and a fourth wing part (5d) extending vertically at the rear end of the lateral fuselage.

    摘要翻译： 一种飞行器，包括由机翼（4），至少一个推进装置和两个侧翼（5）连接的至少两个侧机身（2），所述侧机身分别从所述侧机身（2）延伸并且分别具有前横截面 其特征在于： - 推进装置（3）由每个侧机身（2）携带并分别驱动螺旋桨（6）的电动机组成， - 高度与 飞机的侧翼（5）和翼展在0.15到0.25之间; - 每个侧翼（5）包括在与翼部（4）相同的平面中延伸的第一翼部分（5a），在第一翼部分（5a）上方垂直延伸并且从前部 （5c）平行于所述第一翼部分（5a）延伸并且通过与所述飞机的所述前平面形成角度而从前部延伸到后部以及第四翼部分（5d）延伸，所述第三翼部分（5c） 在横向机身的后端垂直延伸。