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    • 3. 发明申请
    • WING TIP SHAPE FOR A WING, IN PARTICULAR OF AIRCRAFT
    • 特别是飞机的WING TIP形状
    • US20100019094A1
    • 2010-01-28
    • US12515825
    • 2007-11-21
    • Frank TheurichJan Himisch
    • Frank TheurichJan Himisch
    • B64C23/00
    • B64C23/069Y02T50/164
    • A wing for of aircraft has a wing tip shape that has a profile that extends in the direction of the span of the wing, and across the direction of the span of the wing extends from the wing leading edge to the wing trailing edge. The profile is delimited by a first skin and a second skin, with a winglet, arranged on the wing end. The winglet is substantially planar, and has a transition region arranged between the wing and the winglet, that extends from a connection on the wing to a connection on the winglet. The curvature of the local dihedral can increase in the transition region from a low level or a level of zero at or near the wing intersection in the outboard direction.
    • 用于飞行器的机翼具有翼尖形状,其具有沿翼的跨度方向延伸的轮廓,并且跨越翼的跨度的方向从机翼前缘延伸到翼后缘。 轮廓由第一皮肤和第二皮肤划分,具有布置在翼端上的小翼。 小翼基本上是平面的,并且具有布置在翼和小翼之间的过渡区域,其从机翼上的连接延伸到小翼上的连接。 局部二面体的曲率可以在过渡区域从外侧方向上的翼交点处或附近的低水平或零水平增加。
    • 4. 发明申请
    • Tool, Arrangement, and Method for Manufacturing a Component, Component
    • 工具,布置和制造组件的方法
    • US20090218734A1
    • 2009-09-03
    • US12084751
    • 2006-11-09
    • Ulrich EberthMartin Friedrich
    • Ulrich EberthMartin Friedrich
    • B29C43/56B29C70/34
    • B29C70/48B29C45/02B29C45/14786B29C45/462B29C70/546
    • This application describes a tool, an arrangement, and a method of manufacturing a component. The manufacturing of the component is achieved by a resin transfer from a storage chamber via a transfer line into a working chamber. Before the resin transfer, taking place, for example by a compressed air charging of the storage chamber, the storage chamber is filled with an amount of resin adjusted to the size of the component. furthermore, a semi-finished product, consisting of cut-to-size reinforcement fibers, is inserted into the working chamber that is adjusted to the form of the component to be produced. Storage chamber, transfer line, and working chamber are configured in a one-piece mould casing of the tool. The application further describes a component manufactured by the above-mentioned tool or by the above-mentioned method respectively.
    • 该应用描述了一种工具,一种布置和一种制造组件的方法。 通过从存储室经由输送管线将树脂转移到工作室中来实现部件的制造。 在树脂转移之前,例如通过储存室的压缩空气充填进行,储存室中填充有一定量的树脂,该树脂被调整到部件的尺寸。 此外,将由切割尺寸的增强纤维组成的半成品插入到被调节为待生产的部件的形式的工作室中。 储存室,输送管线和工作室均配置在工具的一体式模具外壳中。 本申请还分别描述了通过上述工具制造的部件或上述方法。
    • 5. 发明授权
    • Resin-transfer-moulding method
    • 树脂转印成型法
    • US09352517B2
    • 2016-05-31
    • US13152496
    • 2011-06-03
    • Ulrich EberthMartin Friedrich
    • Ulrich EberthMartin Friedrich
    • B29C70/48B29C45/14B29C45/46B29C70/54B29C45/02
    • B29C70/48B29C45/02B29C45/14786B29C45/462B29C70/546
    • This application describes a tool, an arrangement, and a method of manufacturing a component. The manufacturing of the component is achieved by a resin transfer from a storage chamber via a transfer line into a working chamber. Before the resin transfer, taking place, for example by a compressed air charging of the storage chamber, the storage chamber is filled with an amount of resin adjusted to the size of the component. Furthermore, a semi-finished product, consisting of cut-to-size reinforcement fibers, is inserted into the working chamber that is adjusted to the form of the component to be produced. Storage chamber, transfer line, and working chamber are configured in a one-piece mould casing of the tool. The application further describes a component manufactured by the above-mentioned tool or by the above-mentioned method respectively.
    • 该应用描述了一种工具,一种布置和一种制造组件的方法。 通过从存储室经由输送管线将树脂转移到工作室中来实现部件的制造。 在树脂转移之前,例如通过储存室的压缩空气充填进行,储存室中填充有一定量的树脂,该树脂被调整到部件的尺寸。 此外,将由切割尺寸的增强纤维组成的半成品插入到被调节成待生产部件形式的工作室中。 储存室,输送管线和工作室均配置在工具的一体式模具外壳中。 本申请还分别描述了通过上述工具制造的部件或上述方法。
    • 6. 发明授权
    • Wing tip shape for a wing, in particular of aircraft
    • 机翼的翼尖形状,特别是飞机
    • US08727285B2
    • 2014-05-20
    • US12515825
    • 2007-11-21
    • Frank TheurichJan Himisch
    • Frank TheurichJan Himisch
    • B64C23/06
    • B64C23/069Y02T50/164
    • A wing for of aircraft has a wing tip shape that has a profile that extends in the direction of the span of the wing, and across the direction of the span of the wing extends from the wing leading edge to the wing trailing edge. The profile is delimited by a first skin and a second skin, with a winglet, arranged on the wing end. The winglet is substantially planar, and has a transition region arranged between the wing and the winglet, that extends from a connection on the wing to a connection on the winglet. The curvature of the local dihedral can increase in the transition region from a low level or a level of zero at or near the wing intersection in the outboard direction.
    • 用于飞行器的机翼具有翼尖形状,其具有沿翼的跨度方向延伸的轮廓,并且跨越翼的跨度的方向从机翼前缘延伸到翼后缘。 轮廓由第一皮肤和第二皮肤划分,具有布置在翼端上的小翼。 小翼基本上是平面的,并且具有布置在翼和小翼之间的过渡区域,其从机翼上的连接延伸到小翼上的连接。 局部二面体的曲率可以在过渡区域从外侧方向上的翼交点处或附近的低水平或零水平增加。
    • 9. 发明授权
    • Docking and undocking of liquid carrying lines to and from a docking body
    • 液体携带线对接和脱离对接体
    • US08262141B2
    • 2012-09-11
    • US11992177
    • 2006-09-20
    • Ulrich EberthMartin FriedrichHans-Martin Krafft
    • Ulrich EberthMartin FriedrichHans-Martin Krafft
    • F16L21/02
    • B08B9/023F16L55/103Y10T137/0391
    • A docking system for docking a liquid stream carrying line to a docking body, includes a line end having a first form that is conically tapered in the direction of flow and a docking interface which is situated on the docking body and has a second form that is conically tapered in the direction of flow. The first conically tapered form and the second conically tapered form are adapted to one another in such a way that, in the docked state, they are mutually set apart in one coupling region by an interspace defined by a sealing ring, concentrically opposing one another. The first conically tapered form is equipped on its periphery with at least one cleaning element, which extends from the first conically tapered form toward the second conically tapered form in order to capture liquid that may accumulate in the interspace.
    • 用于将液体流携带线对接到对接体的对接系统包括具有在流动方向上呈锥形锥形的第一形式的线端和位于对接体上的对接界面,并且具有第二形式, 在流动方向呈锥形锥形。 第一锥形形状和第二锥形形状彼此适配,使得在对接状态下,它们通过由密封环限定的间隙在一个耦合区域中相互分开,同心地彼此相对。 第一锥形锥体在其周边配备有至少一个清洁元件,其从第一锥形形状朝向第二锥形形状延伸,以便捕获可能积聚在间隙中的液体。