-
1.发明授权FLÜGEL MIT EINER KRÜGER-KLAPPE UND EINER SPALTABDECKUNGSVORRICHTUNG UND ENTSPRECHENDES VERFAHREN 有权与KRUGER门和GAP罩装置及相应方法WINGS
公开(公告)号：EP2356021B1
公开(公告)日：2013-04-10
申请号：EP09751819.5
申请日：2009-11-10
-
2.发明公开
公开(公告)号：EP2356021A2
公开(公告)日：2011-08-17
申请号：EP09751819.5
申请日：2009-11-10
摘要： The invention relates to a vane having a regulating flap (1) that can be moved between a retracted position and an extended position and a gap covering device (10) having an adjusting lever (13) and a gap covering flap (11) arranged thereon, having a flow surface (11 a), • wherein the adjusting lever (13) having the gap covering flap (11) is prestressed by a prestressing device (20) into a first position in which the gap covering flap (11) is located in the interior (B) of the vane (F), and • wherein the regulating flap (1) and the adjusting lever (13) having the gap covering flap (11) are coupled mechanically such that when the regulating flap (1) moves into the retracted position thereof, the adjusting lever (1) moves into a second position against the prestress produced by the prestressing device (20), and • wherein the flow surface (11 a) of the gap covering flap (11) in the second position of the adjusting lever (13) runs between the top side (2) of the retracted regulating flap (1) and the vane flow surface (7).
-
公开(公告)号：EP3962810A1
公开(公告)日：2022-03-09
申请号：EP20771850.3
申请日：2020-09-14
发明人： SCHLIPF, Bernhard , GEYER, Norbert
-
公开(公告)号：EP2566754B1
公开(公告)日：2018-07-18
申请号：EP11721427.0
申请日：2011-05-03
发明人： SCHLIPF, Bernhard , HUE, Xavier
IPC分类号： B64C3/56
CPC分类号： B64C3/56
摘要： The invention relates to a wing with an extension in the wingspan direction, in the wing chord direction and in the wing thickness direction for use in an aircraft, with a retractable wing end piece. A mechanical lever system is here used, which can execute a pivoting motion of a wing end piece comprising both a rotational component and a translational component. The lever kinematics here comprises two lever arrangements, for which a respective two hinged devices are provided.
-
5.发明授权VERSTELLMECHANISMUS ZUR KINEMATISCHEN VERSTELLUNG EINES HOCHAUFTRIEBSKÖRPERS SOWIE HOCHAUFTRIEBSSYSTEM MIT EINEM SOLCHEN VERSTELLMECHANISMUS 有权调整机构用于高提升身体的运动调节，高扬程系统，其具有这样的调整
公开(公告)号：EP2473403B1
公开(公告)日：2017-05-17
申请号：EP10752524.8
申请日：2010-09-03
-
公开(公告)号：EP2499043A2
公开(公告)日：2012-09-19
申请号：EP10776950.7
申请日：2010-11-10
IPC分类号： B64C9/02
摘要： Trailing-edge flap system comprising a trailing-edge flap and a movement means, the movement means comprising at least a translatory mover for the translation of the trailing-edge flap and at least a rotational mover for the rotation of the trailing-edge flap.
摘要翻译： 描述了后缘襟翼系统。 后缘皮瓣系统包括后缘皮瓣和移动装置。 运动装置至少包括用于翻转后缘翼片的平移运动器和用于后缘翼片的旋转的至少一个旋转移动器。
-
公开(公告)号：EP2496474A2
公开(公告)日：2012-09-12
申请号：EP10787002.4
申请日：2010-11-05
发明人： HUE, Xavier , SCHLIPF, Bernhard
IPC分类号： B64C9/22
CPC分类号： B64C9/22
摘要： A wing (10a) of an aircraft provided with a main wing (10) and an arrangement of leading edge lifting bodies (13a), which as seen with reference to the incident flow direction (F) are arranged on the leading edge, which are adjustably arranged on the main wing (10) one behind another as seen in the spanwise direction (S-T) of the main wing (10) by means of respectively two positioning devices spaced apart from one another in the spanwise direction (S-T) of the main wing, wherein the wing (10a) has a connecting device (K), which is coupled to each of two adjacent leading edge lifting bodies (13a), wherein the connecting device (K) is executed such that in the event of a fracture of a positioning device of a positioning body external forces acting on the latter are transferred via the respective connecting device (K) to the leading edge lifting bodies (13a) coupled up via the latter.
摘要翻译： 飞机的机翼设有主翼和前缘提升体的布置，如参照入射流动方向所示，前缘提升体布置在前缘上，前缘可调节地布置在主翼上，如前所述 通过分别在主翼的翼展方向上彼此间隔开的两个定位装置，主翼的翼展方向。 机翼具有连接装置，其连接到两个相邻的前缘提升体中的每一个，其中连接装置被构造成使得在定位体的定位装置的断裂的情况下，作用在定位体上的外力被转移 通过相应的连接装置连接到通过其连接的前缘提升体。
-
8.发明授权AERODYNAMICALLY EFFECTIVE WING COMPRISING A LIFT-AUGMENTING FLAP, IN PARTICULAR LEADING EDGE FLAP 有权与提升增益门，尤其是鼻缘襟翼空气动力有效WING
公开(公告)号：EP1890934B8
公开(公告)日：2010-02-17
申请号：EP06762052.6
申请日：2006-06-14
摘要： A lift-augmenting leading edge flap for a carrying wing of an aircraft, wherein the flap comprises an essentially rigid main body which makes a transition from the first side to the second side of the wing the flap being adjustable by a retention- and actuation mechanism coupled between the flap and wing box, between a first, retracted, position and a second, extended, position, wherein the first transition region of the flap is slidable to rest in each position essentially free of any gap, against the first skin of the wing box or against the wing end cover, in relation to the wing end cover.
-
公开(公告)号：EP2344379B1
公开(公告)日：2019-12-11
申请号：EP09744054.9
申请日：2009-10-06
发明人： SCHLIPF, Bernhard , HUE, Xavier
IPC分类号： B64C9/24
-
10.发明授权
公开(公告)号：EP2701975B1
公开(公告)日：2018-05-30
申请号：EP12717709.5
申请日：2012-04-27
发明人： HUE, Xavier , SCHLIPF, Bernhard
IPC分类号： B64C9/22
CPC分类号： B64C9/22 , B64C9/02 , B64C2009/143
摘要： A high lift system for an aircraft includes a basic body, a flap which is movably mounted on the basic body and has a flap edge, and a retaining element. The high lift system is set up to form a gap between the flap edge and the basic body. The retaining element is mounted on a region of the flap close to the flap edge and extends towards the basic body to restrict the distance between the flap edge and the basic body. The retaining element is preferably configured as a linear attachment means. Consequently, a gap dimension between a flap and a basic body can be influenced to restrict flexing effects during loading of the flap and of the basic body.
-
-
-
-
-
-
-
-
-
搜索结果
36 条记录 (耗时 0.012 秒)
