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    Track beam for the cowling of jet engines
    2.
    发明申请
    Track beam for the cowling of jet engines 有权
    用于喷气发动机整流罩的轨道梁

    公开(公告)号：US20070294996A1

    公开(公告)日：2007-12-27

    申请号：US11732026

    申请日：2007-04-02

    申请人： Walter Stephan ,  Roland Zeillinger ,  Andreas Maier

    发明人： Walter Stephan ,  Roland Zeillinger ,  Andreas Maier

    IPC分类号： F02K3/02

    CPC分类号： F02K1/64 ,  F02K1/70 ,  F02K1/80 ,  F05D2300/224 ,  F05D2300/44 ,  F05D2300/603 ,  Y02T50/672

    摘要： Track beams for the cowling of a jet engine for aircraft are formed of a base body with at least one slide for displaceably mounting a thrust reverser of the jet engine. A connection is provided for an inner engine cowling and fittings for detachably and pivotally attaching to a supporting structure or for connecting to another track beam. To provide such a track beam which has a particularly low weight yet, nevertheless, is sufficiently stiff, the base body is formed by a hollow profile section with a substantially closed cross-section. The hollow section is produced of a carbon-fiber-reinforced synthetic material by way of a resin-infusion process. Two flanges are provided on the hollow section of the base body of the track beam for providing a connection to the inner engine cowling.

    摘要翻译： 用于飞行器的喷气发动机的罩的轨道梁由具有至少一个滑块的基体形成，用于可移动地安装喷气发动机的推力反向器。 为内部发动机整流罩和配件提供连接，用于可拆卸地和可枢转地附接到支撑结构或用于连接到另一轨道梁。 为了提供具有特别低重量的这种轨道梁，尽管如此，足够坚硬，基体由具有基本封闭横截面的中空型材部分形成。 中空部通过树脂浸渍法由碳纤维增强合成材料制成。 两个凸缘设置在轨道梁的基体的中空部分上，用于提供与内部发动机罩的连接。

    Carrying or guiding device for aircraft components
    3.
    发明申请
    Carrying or guiding device for aircraft components 有权
    飞机部件的携带或引导装置

    公开(公告)号：US20050082434A1

    公开(公告)日：2005-04-21

    申请号：US10493604

    申请日：2002-09-16

    申请人： Walter Stephan

    发明人： Walter Stephan

    IPC分类号： B64C9/16 ,  B64C1/06

    CPC分类号： B64C9/16 ,  Y02T50/44

    摘要： The invention relates to a carrying or guiding device (1), respectively, for aircraft components, in particular for landing flaps arranged on an aircraft wing, comprising a carrier (2) of a substantially U-shaped section and with substantially parallel side walls (3, 4). To provide such a device which has as low a weight as possible and, moreover, has the required strength properties and is as easy to produce and mount as possible, it is provided that the carrier (2) as well as preferably a cover plate (20) arranged at the open side of the carrier (2) is made of fiber reinforced plastic, in particular of carbon fiber (CF) reinforced plastic. The connection between the carrier (2) and the cover plate (20) and any possible connecting elements (21) is preferably provided by gluing and, possibly, by additional rivet or screw connections.

    摘要翻译： 本发明涉及分别用于飞行器部件，特别是布置在飞行器机翼上的着陆挡板的承载或引导装置（1），其包括大致U形截面的载体（2）和基本上平行的侧壁（ 3，4）。 为了提供这样的具有尽可能低的重量的装置，此外，具有所需的强度性能并且尽可能容易地制造和安装，但是提供载体（2）以及优选的盖板 20）布置在载体（2）的开口侧，由纤维增强塑料，特别是碳纤维（CF）增强塑料制成。 载体（2）和盖板（20）和任何可能的连接元件（21）之间的连接优选地通过胶合并且可能通过附加的铆钉或螺钉连接来提供。

    Overhead luggage container, particularly for airplanes
    4.
    发明申请
    Overhead luggage container, particularly for airplanes 有权
    架空行李箱，特别适用于飞机

    公开(公告)号：US20050040287A1

    公开(公告)日：2005-02-24

    申请号：US10489951

    申请日：2002-09-16

    申请人： Walter Stephan ,  Hermann Filsegger ,  Erich Pamminger

    发明人： Walter Stephan ,  Hermann Filsegger ,  Erich Pamminger

    IPC分类号： B61D37/00 ,  B64D11/00

    CPC分类号： B64D11/003 ,  B61D37/003 ,  Y02T50/46

    摘要： 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)

    摘要翻译： 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）

    Spiral wound gasket
    6.
    发明授权
    Spiral wound gasket 失效
    螺旋缠绕垫圈

    公开(公告)号：US5275423A

    公开(公告)日：1994-01-04

    申请号：US939321

    申请日：1992-09-10

    申请人： Kurt Allen ,  Walter Stephan

    发明人： Kurt Allen ,  Walter Stephan

    IPC分类号： F16J15/12

    CPC分类号： F16J15/125 ,  Y10S277/946 ,  Y10S285/91

    摘要： A spiral wound gasket comprises an annulus constituted by a plurality of superposed turns of a profiled metal strip wound upon itself to form a spiral and, interposed between at least some of said superposed turns, a number of turns of a relatively soft sealant material in strip form, the width of said metal strip being selected so that prior to use the wound metal spiral is essentially flush with the surface of an associated guide ring and the width of the strip of relatively soft sealant material being selected so that prior to use, it projects a significant distance on both sides of the gasket from said superposed metal turns axially of said annulus. The preferred relatively soft sealant material is exfoliated graphite foil or a fluorocarbon resin, unsintered PTFE being particularly preferred. The sealant material preferably projects from the metal spiral to define an overall gasket thickness on the order of 25 to 40 percent greater than that of the guide ring.

    摘要翻译： 螺旋缠绕垫圈包括由多个卷绕在其自身上的成型金属带的叠置构成的环形结构，以形成螺旋形，并且插入在至少一些所述重叠的匝之间，条带中的相对软的密封剂材料的匝数 选择所述金属条的宽度，使得在使用之前，卷绕的金属螺旋基本上与相关联的导向环的表面齐平，并且选择相对软的密封剂材料的条的宽度，使得在使用之前， 在所述垫圈的两侧上从所述叠置的金属件在所述环形空间轴向突出相当远的距离。 优选的相对软的密封剂材料是剥离的石墨箔或氟碳树脂，特别优选未烧结的PTFE。 密封剂材料优选地从金属螺旋突出以限定整体衬垫厚度比引导环的厚度大25至40％。

    Track beam for the cowling of jet engines
    7.
    发明授权
    Track beam for the cowling of jet engines 有权
    用于喷气发动机整流罩的轨道梁

    公开(公告)号：US08136341B2

    公开(公告)日：2012-03-20

    申请号：US11732026

    申请日：2007-04-02

    申请人： Walter Stephan ,  Roland Zeillinger ,  Andreas Maier

    发明人： Walter Stephan ,  Roland Zeillinger ,  Andreas Maier

    IPC分类号： F02K3/02

    CPC分类号： F02K1/64 ,  F02K1/70 ,  F02K1/80 ,  F05D2300/224 ,  F05D2300/44 ,  F05D2300/603 ,  Y02T50/672

    摘要： Track beams for the cowling of a jet engine for aircraft are formed of a base body with at least one slide for displaceably mounting a thrust reverser of the jet engine. A connection is provided for an inner engine cowling and fittings for detachably and pivotally attaching to a supporting structure or for connecting to another track beam. To provide such a track beam which has a particularly low weight yet, nevertheless, is sufficiently stiff, the base body is formed by a hollow profile section with a substantially closed cross-section. The hollow section is produced of a carbon-fiber-reinforced synthetic material by way of a resin-infusion process. Two flanges are provided on the hollow section of the base body of the track beam for providing a connection to the inner engine cowling.

    摘要翻译： 用于飞行器的喷气发动机的罩的轨道梁由具有至少一个滑块的基体形成，用于可移动地安装喷气发动机的推力反向器。 为内部发动机整流罩和配件提供连接，用于可拆卸地和可枢转地附接到支撑结构或用于连接到另一轨道梁。 为了提供具有特别低重量的这种轨道梁，尽管如此，足够坚硬，基体由具有基本封闭横截面的中空型材部分形成。 中空部通过树脂浸渍法由碳纤维增强合成材料制成。 两个凸缘设置在轨道梁的基体的中空部分上，用于提供与内部发动机罩的连接。

    Device for introducing and distributing forces into or inside a luggage compartment
    8.
    发明授权
    Device for introducing and distributing forces into or inside a luggage compartment 有权
    用于将力引入和分配到行李箱内或里面的装置

    公开(公告)号：US07918418B2

    公开(公告)日：2011-04-05

    申请号：US10581275

    申请日：2004-11-04

    申请人： Walter Stephan ,  Erich Pamminger

    发明人： Walter Stephan ,  Erich Pamminger

    IPC分类号： B64D11/00

    CPC分类号： B64D11/003 ,  Y02T50/46

    摘要： A device for introducing forces into a luggage compartment and for transferring and/or distributing the forces and/or stresses in vehicles, particularly in fast traveling vehicles such as aircraft, ground vehicles and watercraft, e.g. express trains, speedboats and the like, has a ceiling-side connecting element arranged between extensions of end-side side walls of the luggage compartment. The device has a simple design and can be economically produced. The invention provides for the introduction of the forces into the luggage compartment via the ceiling-side connecting element, configured, for example, as a strip that distributes forces for stresses.

    摘要翻译： 用于将力引入行李舱并用于传递和/或分配车辆中的力和/或应力的装置，特别是在诸如飞机，地面车辆和船只之类的快速行驶车辆中。 快车，快艇等，具有设置在行李箱的端侧侧壁的延伸部之间的天花板侧连接元件。 该设备具有简单的设计，可经济地生产。 本发明提供了通过天花板侧连接元件将力引入行李箱中，该吊顶侧连接元件例如被配置为分配应力的力的条带。

    Spiral wound gasket
    9.
    发明授权
    Spiral wound gasket 失效
    螺旋缠绕垫圈

    公开(公告)号：US5161807A

    公开(公告)日：1992-11-10

    申请号：US768386

    申请日：1991-09-30

    申请人： Kurt Allen ,  Walter Stephan

    发明人： Kurt Allen ,  Walter Stephan

    IPC分类号： F16J15/12

    CPC分类号： F16J15/125 ,  F16L23/20

    摘要： A spiral wound gasket comprises an annulus constituted by a plurality of superposed turns of a profiled metal strip wound upon itself to form a spiral and, interposed between at least some of said superposed turns, a number of turns of a relatively soft sealant material in strip form, the thickness of said metal strip being selected so that prior to use the wound metal spiral is essentially flush with the surface of an associated guide ring and the thickness of the strip of relatively soft sealant material being selected so that prior to use, it projects a significant distance on both sides of the gasket from said superposed metal turns axially of said annulus. The preferred relatively soft sealant material is exfoliated graphite foil, which projects from the metal spiral to define an overall gasket thickness on the order of 25 to 40% greater than that of the guide ring.

    摘要翻译： 螺旋缠绕垫圈包括由多个卷绕在其自身上的成型金属带的叠置构成的环形结构，以形成螺旋形，并且插入在至少一些所述重叠的匝之间，条带中的相对软的密封剂材料的匝数 选择所述金属条的厚度，使得在使用之前，卷绕的金属螺旋基本上与相关联的导向环的表面齐平，并且选择相对软的密封剂材料的条的厚度，使得在使用之前， 在所述垫圈的两侧上从所述叠置的金属件在所述环形空间轴向突出相当远的距离。 优选的相对软的密封剂材料是从金属螺旋突出的剥离的石墨箔，以限定比引导环大的25至40％的整体衬垫厚度。