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公开(公告)号：US06299109B1
公开(公告)日：2001-10-09
申请号：US09441058
申请日：1999-11-16
Applicant: Walter Anton Stephan , Hermann Filsegger
Inventor： Walter Anton Stephan , Hermann Filsegger
IPC: B64C350
Abstract: There is disclosed a spoiler for wings, in particular of planes, which spoiler is unfoldable during the landing and take-off of the plane or the like and retractable during cruising. In order to provide for enhanced aerodynamic conditions during landing and taking off without deteriorating the aerodynamic conditions during cruising, a structural member preferably made of a composite material and, in particular, carbon fiber reinforced plastic is arranged on the trailing edge of the spoiler, viewed in the direction opposite to the flight direction. The structural member, during landing or taking off, in the unfolded state of the spoiler with the landing flaps extended reduces the gap formed between the trailing edge of the spoiler and the surface of the landing flap and, during cruising, with the landing flap pulled in and the spoiler retracted abuts on the surface of the landing flap.
Abstract translation: 公开了一种用于机翼，特别是飞机的扰流板，该扰流板在飞机着陆和起飞期间是可展开的，并且可以在巡航期间缩回。 为了在着陆和起飞期间提供增强的空气动力学条件，而不会在巡航期间的空气动力学条件恶化，优选地由复合材料制成的结构构件，特别是碳纤维增强塑料布置在扰流板的后缘，观察 在与飞行方向相反的方向上。 结构构件在着陆或起飞期间处于展开状态下的带有着陆襟翼的扰流板，减少了扰流板的后缘与着陆挡板表面之间形成的间隙，并且在巡航期间，着陆挡板被拉 并且扰流器缩回邻接在着陆挡板的表面上。
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公开(公告)号：US07258406B2
公开(公告)日：2007-08-21
申请号：US10491723
申请日：2002-09-23
Applicant: Walter Alfred Stephan , Hermann Filsegger
Inventor： Walter Alfred Stephan , Hermann Filsegger
CPC classification number: B64D11/003 , B60R5/003 , B61D37/003
Abstract: A suspension device for a lowerable luggage stowage compartment has at least one spring element for assisting the movement of the compartment into a closed position against the force of gravity, and at least one damping element for damping the movement of the compartment into an opened position. A weight detector detects the weight of the compartment, and at least one additional spring element can be actuated based on the detected weight of the compartment. A retention device is provided for fixing the additional spring element. The suspension device provides a compartment that is easy to handle and easy to close even when fully loaded.
Abstract translation: 用于可下降行李存放舱的悬挂装置具有至少一个弹簧元件，用于帮助隔室抵抗重力的作用使舱室移动到关闭位置;以及至少一个阻尼元件，用于阻止隔室的运动进入打开位置。 重量检测器检测隔室的重量，并且可以基于检测到的隔室的重量来致动至少一个附加弹簧元件。 提供了用于固定附加弹簧元件的保持装置。 悬挂装置提供容易处理并且即使在满载时易于关闭的隔间。
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公开(公告)号：US20050040287A1
公开(公告)日：2005-02-24
申请号：US10489951
申请日：2002-09-16
Applicant: Walter Stephan , Hermann Filsegger , Erich Pamminger
Inventor： Walter Stephan , Hermann Filsegger , Erich Pamminger
CPC classification number: B64D11/003 , B61D37/003 , Y02T50/46
Abstract: The invention relates to an overhead luggage container (1), particularly for airlines, comprising a reinforcing structure (11) which is connected to the container (1) and which is disposed essentially in the direction of the longitudinal extension of the container (1), and at least one device (5) for suspension on a carrying structure (2) of the plane or like. In order to create a container (1) which can be subjected to relatively high static strain without running the risk that the container (1) will fall on the passengers sitting below, while at the same time reducing technical complexity in production and reducing the weight of said container, at least one respective rigid connecting element (17) is arranged to the side of the container (1) between the reinforcing structure (11) and the suspension device (5) in a substantially vertical manner with respect to the longitudinal extension of the container (1). The connecting element (17) is used to transmit forces exerted by the luggage on said container (1) and to deflect them to the suspension devices (5) and carrying structure (2) of the plane, thereby relieving the amount of strain placed on the side walls (12)
Abstract translation: 本发明涉及一种特别用于航空公司的高架行李箱容器（1），其包括连接到容器（1）并且基本上沿容器（1）的纵向延伸方向设置的加强结构（11） ，以及用于悬挂在该平面等的承载结构（2）上的至少一个装置（5）。 为了形成容器（1），可容纳相对较高的静态应变，而不会发生容器（1）落在坐在下方的乘客身上的风险，同时降低了生产中的技术复杂性并降低了重量 所述容器的至少一个相应的刚性连接元件（17）以相对于所述容器的纵向延伸部基本垂直的方式布置在所述加强结构（11）和所述悬挂装置（5）之间的所述容器（1） 的容器（1）。 连接元件（17）用于将由行李施加的力传递到所述容器（1）上并将其偏转到悬挂装置（5）并承载平面的结构（2），从而减轻施加在 侧壁（12）
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Patent Agency Ranking
公开(公告)号：US06227491B1
公开(公告)日：2001-05-08
申请号：US09122716
申请日：1998-07-27
Applicant: Walter A. Stephan , Hermann Filsegger
Inventor： Walter A. Stephan , Hermann Filsegger
IPC: B64C114
CPC classification number: B64C1/1492
Abstract: The invention relates to a window unit W for aircraft cabins, comprising an outer window frame 1, an inner window frame 3, a window pane 2 lying between them, and possibly having a sun-visor 4, a roller blind 34 or the like arranged between the inner window frame 3 and a possible covering frame 5, the window unit W being insertable into the opening 7 in a side-wall panel 6 or the like in the aircraft cabin. In order to make it possible for the window unit W to be rapidly and simply installed and removed, the invention makes provision for the window unit W to have a centering device and at least two snap fastenings 13, advantageously with locking devices, to detachably connect it to the side-wall panel 6, or to components connected thereto, the side-wall panel 6, or components connected thereto, having any necessary mating parts for the centering device for the snap fastenings 13. The centering device is advantageously arranged corresponding to a clock position of 6 o'clock, and two snap fastenings 13 are advantageously arranged on the circumference of the window unit (W) corresponding to a clock position of 10 and 2 o'clock.
Abstract translation: 本发明涉及一种用于飞机机舱的窗单元W，其包括外窗框架1，内窗框架3，位于它们之间的窗玻璃2，并且可能具有遮阳板4，卷帘34等 在内窗框架3和可能的覆盖框架5之间，窗单元W可插入飞机机舱中的侧壁板6等中的开口7中。 为了使窗单元W能够快速且简单地安装和拆卸成为可能，本发明提供了将窗单元W设置成具有定心装置和至少两个卡扣紧固件13，有利地具有锁定装置，以可拆卸地连接 侧壁板6或与其连接的部件，侧壁板6或与其连接的部件，具有用于卡扣紧固件13的定心装置的任何必要的配合部件。定心装置有利地布置成对应于 六点钟的时钟位置和两个卡扣紧固件13有利地布置在对应于10点钟和2点钟的时钟位置的窗口单元（W）的圆周上。
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公开(公告)号：US07097138B2
公开(公告)日：2006-08-29
申请号：US10489951
申请日：2002-09-16
Applicant: Walter Alfred Stephan , Hermann Filsegger , Erich Pamminger
Inventor： Walter Alfred Stephan , Hermann Filsegger , Erich Pamminger
IPC: B64C11/06
CPC classification number: B64D11/003 , B61D37/003 , Y02T50/46
Abstract: The invention relates to an overhead luggage container (1), particularly for airlines, comprising a reinforcing structure (11) which is connected to the container (1) and which is disposed essentially in the direction of the longitudinal extension of the container (1), and at least one device (5) for suspension on a carrying structure (2) of the plane. In order to create a container (1) which can be subjected to relatively high static strain without running the risk that the container (1) will fall on the passengers sitting below, while at the same time reducing technical complexity in production and reducing the weight of the container, at least one respective rigid connecting element (17) is arranged to the side of the container (1) between the reinforcing structure (11) and the suspension device (5) in a substantially vertical manner with respect to the longitudinal extension of the container (1). The connecting element (17) is used to transmit forces exerted by the luggage on the container (1) and to deflect them to the suspension devices (5) and carrying structure (2) of the plane, thereby relieving the amount of strain placed on the side walls (12).
Abstract translation: 本发明涉及一种特别用于航空公司的高架行李箱容器（1），其包括连接到容器（1）并且基本上沿容器（1）的纵向延伸方向设置的加强结构（11） ，以及用于悬挂在该平面的承载结构（2）上的至少一个装置（5）。 为了形成容器（1），可容纳相对较高的静态应变，而不会发生容器（1）落在坐在下方的乘客身上的风险，同时降低了生产中的技术复杂性并降低了重量 容器的至少一个相应的刚性连接元件（17）以相对于纵向延伸部的大致垂直方式设置在加强结构（11）和悬挂装置（5）之间的容器（1）侧上 的容器（1）。 连接元件（17）用于将由行李施加的力传递到容器（1）上并将其偏转到悬挂装置（5）和承载结构（2），从而减轻施加在 侧壁（12）。
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公开(公告)号：US06199798B1
公开(公告)日：2001-03-13
申请号：US09111060
申请日：1998-07-07
Applicant: Walter A. Stephan , Hermann Filsegger
Inventor： Walter A. Stephan , Hermann Filsegger
IPC: B64C114
Abstract: A device for releasably fastening covering panels, in particular ceiling panels in aircraft, on a load-bearing structure, having at least two fastening elements. In order to make it possible for the covering panels to be removed and fastened quickly and easily without the aid of tools, and for loose constituent parts to be avoided, it is provided that all the constituent parts of the fastening elements are connected either to the covering panel and/or to the load-bearing structure, and that all those constituent parts of the fastening elements which are connected to the covering panel are arranged exclusively on that side of the covering panel which is directed toward the load-bearing structure, and that at least one fastening element is designed as a movable bearing, e.g. as a bolt, for absorbing the forces which act essentially perpendicularly with respect to the covering panel, and at least one fastening element is designed as a fixed bearing, e.g. as a bolt, for additionally absorbing the forces which act essentially in the direction of the covering panel, and that each fastening element which is designed as a fixed bearing has means for tool-free locking and unlocking.
Abstract translation: 一种用于将具有至少两个紧固元件的覆盖板，特别是飞行器中的天花板板可释放地紧固在承载结构上的装置。 为了能够在没有工具的情况下快速且容易地移除和紧固覆盖板，并且为了避免组装部件松动，可以将紧固元件的所有组成部分连接到 覆盖板和/或承载结构，并且连接到覆盖板的紧固元件的所有构成部分排列在指向承重结构的覆盖板的侧面上，以及 至少一个紧固元件被设计为可移动轴承，例如 作为螺栓，用于吸收相对于覆盖板基本上垂直地作用的力，并且至少一个紧固元件被设计为固定轴承，例如固定轴承。 作为螺栓，用于另外吸收基本上沿着覆盖板的方向作用的力，并且被设计为固定轴承的每个紧固元件具有用于无工具的锁定和解锁的装置。
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公开(公告)号：US06378805B1
公开(公告)日：2002-04-30
申请号：US09530582
申请日：2000-05-09
Applicant: Walter Stephan , Hermann Filsegger
Inventor： Walter Stephan , Hermann Filsegger
IPC: B64C110
CPC classification number: B64C1/10
Abstract: A pressure frame, designed in particular for an aircraft, including a dome-shaped cover made of composite materials reinforced with fibers, preferably in one single piece, and cover reinforcing devices connected to the cover or produced integrally therewith. To reduce weight and cost while still fulfilling strain requirements, particularly of large aircraft, and to reduce the risk of destruction due to the cover being turned inside out towards the inside of the aircraft, the cover is of essentially uniform thickness and includes at least one cover reinforcing device which is mounted in the central area on the concave side of the cover. Advantageously, this cover reinforcing device in the central area is formed by a reinforcing structure oriented against the curvature of the cover, such as at truncated cone-shaped, mug-shaped or parabolic structure, with a cavity being arranged between the cover and the reinforcing structure.
Abstract translation: 一种特别设计用于飞机的压力框架，包括由纤维增强的复合材料制成的圆顶形盖，优选地在一个单件中，并且覆盖连接到盖或与其一体制造的加强装置。 为了减轻重量和成本，同时仍然满足应变要求，特别是大型飞机的应变要求，并且为了降低由于盖向内转向飞行器内部而导致的破坏的风险，盖体基本上是均匀的厚度，并且包括至少一个 覆盖加强装置，其安装在盖的凹面侧的中央区域。 有利地，中心区域中的该覆盖物加强装置由抵抗盖的曲率取向的加强结构形成，例如截锥形，杯形或抛物线结构，其中空腔布置在盖和加强件之间 结构体。
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公开(公告)号：US6164592A
公开(公告)日：2000-12-26
申请号：US110952
申请日：1998-07-07
Applicant: Walter A. Stephan , Hermann Filsegger
Inventor： Walter A. Stephan , Hermann Filsegger
CPC classification number: E05F1/1215 , E05F1/1223 , E05F3/14 , E05F3/16 , E05F3/20 , E05F5/06 , E05Y2201/21 , E05Y2201/254 , E05Y2201/256 , E05Y2201/266 , E05Y2900/502 , Y10T16/5381
Abstract: In order to provide a container 1 having a door 2, in particular a luggage compartment for aircraft, the door 2 being mounted via at least one hinge or the like on the container 1 such that it can pivot, having an apparatus for assisting the movement of the door 2 into the open position and for holding the door 2 in the open position, and having an apparatus for holding the door 2 in the closed position, in the case of which container the structural components have as small a physical size as possible and thus occupy as little volume in the container 1 as possible. It is provided that the apparatus for assisting the movement of the door 2 and, possibly, an apparatus for damping the movement of the door 2 are arranged essentially around the pivoting axis of the door 2. The components relating to this are ideally integrated in the or each hinge. The damping of the movement of the door 2 advantageously reduces as the opening angle .alpha. of the door 2 increases or as the rate at which the door 2 is opened reduces.
Abstract translation: 为了提供具有门2的容器1，特别是用于飞行器的行李舱，门2通过至少一个铰链等安装在容器1上，使得其可以枢转，具有用于辅助移动的装置 的门2进入打开位置并且将门2保持在打开位置，并且具有用于将门2保持在关闭位置的装置，在这种情况下，结构部件具有尽可能小的物理尺寸 从而在容器1中尽可能少地占有体积。 提供用于辅助门2的移动的装置以及可能的用于阻止门2的运动的装置基本上围绕门2的枢转轴线布置。与此相关的部件理想地集成在 或每个铰链。 门2的运动的阻尼有利地随着门2的打开角度α增加或者打开门2的速度减小而减小。
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