-
公开(公告)号：EP3683140A1
公开(公告)日：2020-07-22
申请号：EP19152669.8
申请日：2019-01-18
申请人： Asco Industries NV
摘要： A slat for an aircraft wing and a method for assembling said slat, the slat comprising:
- a skin wherein an outer surface of the skin forms an aerodynamic surface of the slat body and wherein the skin comprises an upper skin part and a lower skin part extending continuously from a leading edge of the skin such that the upper skin part extends further than the lower skin part seen in a direction along a center line of the slat;
- a plurality of stiffeners are assembled to an inner surface of the skin;
- a spar extending between the upper skin part and the lower skin part that is connected to the upper skin part and the lower skin part;
- wherein the spar is provided with lugs for connection to an actuation system.-
公开(公告)号：EP3501977A1
公开(公告)日：2019-06-26
申请号：EP17208661.3
申请日：2017-12-19
申请人： Asco Industries NV
摘要： Deployment system for adjusting a leading edge high lift device, in particular a slat, between a retracted position, in which, in use, the high lift device is retracted with respect to an airfoil, and at least one deployed position, in which, in use, the high lift device is deployed with respect to the airfoil, comprising at least one actuation unit that is configured to actuate the high lift device between the retracted position and the at least one deployed position, at least one guidance unit that is configured to guide the high lift device during adjustment between the retracted position and the at least one deployed position along an adjustment path, wherein the guidance unit is independent from the actuation unit.
-
公开(公告)号：EP3395678A1
公开(公告)日：2018-10-31
申请号：EP17168255.2
申请日：2017-04-26
申请人： Asco Industries NV
发明人： Vervliet, Antoon Marcel , Paulus, Ivo Peter Marie , Verhuizen, Alexander Jean M. , Janssens, Stein
IPC分类号： B64C9/22
摘要： Guidance assembly for guiding a movement of an airfoil leading edge high-lift device carrier track between a retracted position and an extended position, comprising at least one lower guide element contacting a lower surface of said carrier track and/or at least one upper guide element contacting an upper surface of said carrier track, wherein at least one of said lower or upper guide elements includes a sliding surface arranged to be in sliding contact with said high-lift device carrier track during movement of said carrier track.
-
公开(公告)号：EP3378759A1
公开(公告)日：2018-09-26
申请号：EP17162649.2
申请日：2017-03-23
发明人： Vervliet, Antoon Marcel , Raets, Michaël , Quettier, Gaël Thierry Eric Maurice Ghislain , Wild, Jochen Wolfram , Everaert, Bob Armand Henri
摘要： Airfoil trailing edge high-lift device comprising at least one flap, wherein said flap is movable between a retracted position and at least one deployed position, and is arranged to be actuated by an actuation system comprising at least one rib which is mountable to an airfoil, wherein the rib comprises a track along which the trailing edge high-lift device is adjustable between a retracted position in which the trailing edge high-lift device is substantially partly inside the airfoil, and at least one deployed position in which the trailing edge high-lift device is substantially outside of the airfoil; comprising an adjustment mechanism arranged to adjust the trailing edge high-lift device along the track.
-
公开(公告)号：EP4286271A1
公开(公告)日：2023-12-06
申请号：EP22176859.1
申请日：2022-06-01
申请人： Asco Industries NV
IPC分类号： B64C9/16
摘要： Actuation assembly for a trailing edge flap of an aircraft wing, comprising: a track fixable to the aircraft wing; a carriage arranged on the track so as to be movable across a range of carriage positions along the track; a flap-to-carriage connector configured to hingeably connect the carriage to a leading edge of the flap so as to determine a flap-to-carriage hinging axis extending transverse to a main track direction of the track at the leading edge of the flap; and a first actuator configured to controllably rotate the flap with respect to the carriage about the flap-to-carriage hinging axis, wherein the actuation assembly is configured to enable the flap, when connected, to be adjusted with respect to the wing between a retracted flap position and an extended flap position by moving the carriage within the range of carriage positions along the track.
-
公开(公告)号：EP4140877A1
公开(公告)日：2023-03-01
申请号：EP22200637.1
申请日：2019-01-18
申请人： Asco Industries NV
摘要： Method for assembling a slat, for an aircraft wing, comprising providing a skin and a plurality of stiffeners; assembling the stiffeners to the skin obtaining a skin sub-assembly; providing a spar and a plurality of lugs; assembling the lugs to the spar obtaining a spar sub-assembly; assembling the spar sub-assembly to the skin sub-assembly to obtain the slat.
-
公开(公告)号：EP3231702A1
公开(公告)日：2017-10-18
申请号：EP16173405.8
申请日：2016-06-07
申请人： Asco Industries NV
发明人： Everaert, Bob Armand Henri , Verhuizen, Alexander Jean M. , Thys, Raf , De Baere, Tom Robert Adelin , Raets, Michaël
摘要： A high-lift device (1) comprising an airfoil shaped body (2) having a leading edge and a trailing edge and extending in a spanwise direction configured mainly to generate aerodynamic force; a profile structure (9) arranged to be mounted inside of the airfoil shaped body and extending in spanwise direction of the airfoil shaped body that is configured to provide most of the mechanical strength and stiffness; wherein the airfoil shaped body (2) is provided with an opening (7) extending in spanwise direction at one side through which the profile structure (9) can be fastened and remains accessible inside of the airfoil shaped body.
摘要翻译： 1。一种高升力装置（1），包括：翼型体（2），所述翼型体具有前缘和后缘，并且沿展向方向延伸，主要构造成产生空气动力; 所述型材结构（9）被布置成安装在所述翼型体的内部并且在所述翼型体的展向方向上延伸，所述翼型体的展向方向被构造成提供大部分的机械强度和刚度; 其中所述翼型体（2）设置有开口（7），所述开口沿翼展方向在一侧延伸，所述型材结构（9）能够通过所述开口紧固并且在所述翼型体内保持可接近。
-
-
-
-
-
-
搜索结果
7 条记录 (耗时 0.009 秒)
