公开(公告)号：US20090317246A1

公开(公告)日：2009-12-24

申请号：US12306955

申请日：2007-06-29

Applicant: Andreas Lutz ,  Thomas Wettemann

Inventor： Andreas Lutz ,  Thomas Wettemann

IPC: F01D9/04

CPC classification number: F04D29/542 ,  F01D5/14 ,  F01D5/282 ,  F01D9/042 ,  F01D25/246 ,  F04D29/644 ,  F05D2300/43 ,  F05D2300/603 ,  F05D2300/614 ,  Y02T50/672 ,  Y02T50/673

Abstract: The invention relates to a guide-vane arrangement (1) for deviating the flow present in the by-pass flow channel (2) of an engine (3), said arrangement comprising an outer ring (4) and an inner ring (5) and guide vanes (6) arranged therebetween in a substantially radial manner, wherein the outer ring (4) has elements (7) for connecting to an outer engine structure (8), and the inner ring (5) has elements (9) for connecting to an inner engine structure (10), with a plurality of segments (11) being provided. In order to create a guide-vane arrangement (1) which is sufficiently stable and has optimum aerodynamic properties, each segment (11) is integrally produced from at least one guide vane (6) with a part (12) of the outer ring (4) having at least two flanges (14) for fixing to the outer engine structure (8), and with a part (13) of the inner ring (5) having at least two flanges (15) for fixing to the inner engine structure (10), the segments (11) preferably being made of fiber-reinforced plastic composite material, preferably by an RTM (resin transfer molding) method.

Abstract translation: 本发明涉及用于使存在于发动机（3）的旁通流动通道（2）中的流动偏离的导向叶片装置（1），所述装置包括外环（4）和内圈（5） 和引导叶片（6），其基本上径向地布置在其间，其中所述外环（4）具有用于连接到外部发动机结构（8）的元件（7），并且所述内圈（5）具有用于 连接到内部发动机结构（10），其中设置有多个段（11）。 为了形成足够稳定且具有最佳空气动力特性的导向叶片装置（1），每个段（11）由至少一个导向叶片（6）与外环的一部分（12）整体地产生 4）具有用于固定到外部发动机结构（8）的至少两个凸缘（14），并且内圈（5）的一部分（13）具有至少两个凸缘（15），用于固定到内部发动机结构 （10）中，段（11）优选地由纤维增强塑料复合材料制成，优选通过RTM（树脂传递模制）方法。

公开(公告)号：US07011276B2

公开(公告)日：2006-03-14

申请号：US10493604

申请日：2002-09-16

Applicant: Walter Alfred Stephan

Inventor： Walter Alfred Stephan

IPC: B64C9/02

CPC classification number: B64C9/16 ,  Y02T50/44

Abstract: A carrying or guiding device for aircraft components, in particular for landing flaps arranged on an aircraft wing, including a carrier having a substantially U-shaped section with substantially parallel side walls, and a cover plate arranged at the open side. To minimize weight, facilitate manufacture and mounting, and provide sufficient strength, the carrier and the cover plate are made of fiber reinforced plastic, in particular of carbon fiber (CF) reinforced plastic. The connection between the carrier and the cover plate and any possible connecting elements is preferably provided by gluing and, possibly, by additional rivet or screw connections.

Abstract translation: 用于飞机部件的搬运或引导装置，特别是用于设置在飞行器机翼上的着陆挡板，包括具有基本上U形截面的具有基本上平行的侧壁的载体以及布置在开放侧的盖板。 为了最小化重量，便于制造和安装，并提供足够的强度，载体和盖板由纤维增强塑料，特别是碳纤维（CF）增强塑料制成。 载体和盖板与任何可能的连接元件之间的连接优选通过胶合和可能地通过附加的铆钉或螺钉连接来提供。

公开(公告)号：US20080099615A1

公开(公告)日：2008-05-01

申请号：US11801960

申请日：2007-05-11

Applicant: Gottfried Steiner ,  Mario Staubmann

Inventor： Gottfried Steiner ,  Mario Staubmann

IPC: B64C1/14

CPC classification number: B64C1/1484

Abstract: A modular aircraft window includes an outer pane and an inner pane each inserted in a substantially rectangular frame. A foldable shade is disposed on one of the frames and has a freely movable end that is coupled with an operating unit for opening and closing the shade. The assembly further includes at least one shade raising and lowering mechanism in one or both of the longitudinal parts of the frame and a drive mechanism mounted in the lower transverse part of the frame. The drive mechanism includes a threaded spindle which, in order to provide for a particularly stable and long-lasting construction of the drive mechanism, is movable solely translationally and is coupled with a transmission mechanism operating the at least one raising and lowering mechanism.

Abstract translation: 模块化飞机窗口包括每个插入大致矩形框架的外窗格和内窗格。 一个可折叠的遮光罩设置在其中一个框架上，并且具有可自由移动的端部，该端部与用于打开和关闭遮光罩的操作单元联接。 该组件还包括在框架的一个或两个纵向部分中的至少一个升降机构以及安装在框架的下横向部分中的驱动机构。 驱动机构包括螺纹主轴，为了提供驱动机构的特别稳定和持久的构造，其可以单独平移地移动并且与操作至少一个升降机构的传动机构联接。

公开(公告)号：US20070294996A1

公开(公告)日：2007-12-27

申请号：US11732026

申请日：2007-04-02

Applicant: Walter Stephan ,  Roland Zeillinger ,  Andreas Maier

Inventor： Walter Stephan ,  Roland Zeillinger ,  Andreas Maier

IPC: F02K3/02

CPC classification number: F02K1/64 ,  F02K1/70 ,  F02K1/80 ,  F05D2300/224 ,  F05D2300/44 ,  F05D2300/603 ,  Y02T50/672

Abstract: 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.

Abstract translation: 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。

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

IPC: A47F5/08 ,  B64D11/00

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。