-
公开(公告)号：EP1984646A1
公开(公告)日：2008-10-29
申请号：EP07711464.3
申请日：2007-02-07
IPC分类号： F16F7/12
CPC分类号： F16F7/123
摘要： These days, typically strong holders for attachment of inboard devices to the primary structure of an aircraft are used, which often only ineffectively manage dynamic loads. According to an exemplary embodiment of the present invention, an energy absorber is provided for aircraft, which includes one or more energy absorber elements and a housing, whereby the energy absorber elements can absorb crash impulses by plastic deformation within the housing. Thus, the load on the primary structure is limited, which can lead to an increased, passive safety of the passengers and a weight reduction.
-
公开(公告)号：EP1984645A1
公开(公告)日：2008-10-29
申请号：EP07703165.6
申请日：2007-01-31
摘要： These days, typically strong holders for attachment of inboard devices to the primary structure of an aircraft are used, which may often only ineffectively manage dynamic loads . According to an exemplary embodiment of the present invention, a force level control for an energy absorber (100) is provided for aircraft, which includes an adjustment element (801) and a housing 101;102) , whereby via the adjustment element, a bending radius of the energy absorber element (102) is continuously adjustable in the housing.
-
公开(公告)号：EP1984245A1
公开(公告)日：2008-10-29
申请号：EP07703357.9
申请日：2007-02-08
IPC分类号： B64D11/00
摘要： These days, typically strong holders for attachment of inboard devices to the primary structure of an aircraft are used, which often only ineffectively manage dynamic loads. According to an exemplary embodiment of the present invention, an energy absorber is provided for aircraft, which includes one or more energy absorber elements and a housing, whereby the energy absorber elements can absorb crash impulses by plastic deformation within the housing. Thus, the load on the primary structure is limited, which can lead to an increased, passive safety of the passengers and a weight reduction.
摘要翻译： 目前，通常使用坚固的固定器来将内侧装置固定在飞机的主要结构上，这往往只能无效地管理动态载荷。 根据本发明的示例性实施例，为飞机提供能量吸收器，其包括一个或多个能量吸收器元件和壳体，由此能量吸收器元件可以通过壳体内的塑性变形来吸收碰撞冲击。 因此，主结构上的载荷是有限的，这可能导致乘客的被动安全性增加和重量减轻。
-
4.发明公开ARRANGEMENT OF LINE CONNECTIONS FOR INSTALLATIONS IN AN AIRCRAFT PASSENGER CABIN 有权线的连接安排IN A平面客舱植物
公开(公告)号：EP1848631A1
公开(公告)日：2007-10-31
申请号：EP06706946.8
申请日：2006-02-14
发明人： GONNSEN, Johannes , FOKKEN, Markus , DUPONT, Michael , HARRIEHAUSEN, Michael , LEHMANN, Lars , SCHEEL, Marc , REPP, Stefan
CPC分类号： B64D11/00 , B64D11/02 , B64D11/04 , Y10T137/6906
摘要： The present invention relates to an arrangement of line connections (6, 6' , 6') for installations in an aircraft passenger cabin. The arrangement comprises a line connection element for accommodating several line connections; wherein the line connection element (6, 6' , 6') has a fixed position in the floor grid; wherein the line connections are adaptable to system lines (7-11) of aircraft systems; and wherein the installations are adaptable by way of flexible inlet lines (14, 14' , 15, 15') on the line connection element.
-
-
-
搜索结果
4 条记录 (耗时 0.01 秒)
