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    • 1. 发明授权
    • Actuator for generating high regulating forces and large regulating
distances
    • 用于产生高调节力和大调节距离的执行器
    • US5860352A
    • 1999-01-19
    • US816269
    • 1997-03-13
    • Arno PabschMatthias PieningThilo Bein
    • Arno PabschMatthias PieningThilo Bein
    • F15B15/10F01B19/00
    • F15B15/103
    • The invention relates to an actuator (10) for generating high regulating forces and large regulating distances with a web (12) for the transmission of regulating forces, which actuates an internal pressure, which may be purposefully influenced, in an actuator cavity (14), sealed at least in an indirectly pressure-tight manner, wherein a tubular cavity profile (13) forms the active actuator cavity (14), the shell surface of which is heavily indented in linear form in the effective direction (11) of the regulating forces and in the longitudinal direction of the cavity profile (13) to receive and operate the web (12), and the cavity profile (13) is divided into two mirror-symmetric partial cross-sectional faces (15).
    • 本发明涉及一种致动器(10),用于产生用于传递调节力的幅材(12)的高调节力和大的调节距离,所述调节力致动在致动器空腔(14)中可能有目的地影响的内部压力, 至少以间接压力密封的方式密封,其中管状空腔型材(13)形成主动致动器空腔(14),其壳体表面在调节的有效方向(11)上以线性形式大量缩进 并且在空腔型材(13)的纵向方向上容纳和操作幅材(12),并且空腔轮廓(13)被分成两个镜对称的部分横截面(15)。
    • 2. 发明授权
    • Aircraft with supporting wings having members for taking up tensile and
compressive forces
    • 具有支撑翼的飞机具有用于承受拉伸和压缩力的构件
    • US5924649A
    • 1999-07-20
    • US694817
    • 1996-08-09
    • Matthias PieningArno PabschChristof Sigle
    • Matthias PieningArno PabschChristof Sigle
    • B64C1/26B64C3/20B64C3/56
    • B64C3/20B64C1/26B64C3/56
    • An aircraft with supporting wings including wing shells with good shear strength made of fibrous composite materials, particularly fiber-reinforced plastics, having members taking up tensile and compressive forces on the inside of the wing shells. The members have unidirectional fibers extending longitudinally of the wing, and fixing elements which can be joined detachably to fuselage attachments are provided on the members at the root end of the wing. Stringers are constructed on the inside of the wing shells and spaced longitudinally of the shells, their fiber component being formed by a fiber layer joined to the fiber layer of the wing shell. Fiber bundles are arranged between spaced stringers as unidirectional stiffening elements. The fiber bundles are embedded in the synthetic resin matrix of the plane load-bearing structure and extend longitudinally of the supporting wing. Groups of three fiber bundles extending adjacent each other are provided, of which the two outer bundles in each case form a loop at the root of the supporting wing to receive a bolt which has to be inserted in the loop perpendicular to the plane of the two fiber bundles. The inner bundle is turned down to form a second loop perpendicular to the first loop to receive a bolt which has to be inserted in and perpendicular to the plane of this loop. Both bolts act as connection members to attachment members on the fuselage.
    • 具有支撑翼的飞机包括由纤维复合材料制成的具有良好剪切强度的翼壳,特别是纤维增强塑料,具有在翼壳内部承受拉伸和压缩力的构件。 这些构件具有沿着机翼纵向延伸的单向纤维,并且可以可拆卸地连接到机身附件的固定元件设置在机翼的根部的构件上。 纵梁构造在机翼壳体的内侧并且在壳体纵向间隔开,它们的纤维部件由连接到翼壳的纤维层的纤维层形成。 纤维束布置在间隔桁条之间,作为单向加强元件。 纤维束嵌入在平面承载结构的合成树脂基体中并且在支撑翼的纵向上延伸。 提供了彼此相邻延伸的三个纤维束的组,其中两个外部束在每种情况下在支撑翼的根部处形成环,以接收必须插入在垂直于两个平面的平面的环中的螺栓 纤维束。 内束被向下转动以形成垂直于第一环的第二环,以接收必须插入并垂直于该环的平面的螺栓。 两个螺栓作为机身上的连接构件的连接构件。
    • 3. 发明授权
    • Aircraft wing
    • 飞机机翼
    • US5735486A
    • 1998-04-07
    • US696029
    • 1996-08-09
    • Matthias PieningArno PabschChristof Sigle
    • Matthias PieningArno PabschChristof Sigle
    • B64C3/20B64C3/18B64C11/20F01D5/14
    • B64C3/20
    • In a wing with wing shells with good shear strength made of fibrous composite materials, particularly fiber-reinforced plastics, for aircraft, members taking up tensile and compressive forces are attached to the inside of the wing shells. These members have unidirectional fibers extending longitudinally of the wing. Stringers spaced longitudinally of the wing are provided on the inside of the wing shells, their fiber component being formed by a fiber ply joined to the fiber ply of the wing shell. Unidirectional fibre bundles are arranged between spaced stringers, the bundles being embedded with good shear strength in the synthetic resin matrix of the wing shells, extending longitudinally of the wing and having a substantially rectangular cross-section.
    • 在具有由纤维复合材料,特别是纤维增强塑料制成的具有良好剪切强度的翼壳的机翼中,对于飞行器,承载拉伸和压缩力的构件附接到翼壳的内部。 这些构件具有沿机翼纵向延伸的单向纤维。 在机翼壳体的内侧设有沿机翼纵向隔开的横梁,它们的纤维部件由连接到翼壳的纤维层的纤维层构成。 单向纤维束布置在间隔的桁条之间,该束在翼壳的合成树脂基体中被嵌入具有良好的剪切强度,在翼的纵向延伸并且具有基本矩形的横截面。
    • 5. 发明授权
    • Apparatus for making components of large area by RTM
    • 通过RTM制造大面积部件的装置
    • US06257858B1
    • 2001-07-10
    • US09043977
    • 1998-06-19
    • Arno PabschChristof SigleMatthias Piening
    • Arno PabschChristof SigleMatthias Piening
    • B29C7044
    • B29C70/548B29C70/443B29C70/48B29L2007/002B29L2031/3085
    • In a process for producing large-surface structural elements from fiber-reinforced composite materials by resin transfer moulding, a mold (2) that can be evacuated has a dimensionally stable part (4) and an elastically deformable part (6). The mold (2) has connections for injecting a resin mixture and connections to a pressure sink. A fibrous fabric (12) is set into the mold (2). Elongated pipes having a large supporting surface (22) and a cavity (24) that extends in the longitudinal direction of the pipes above the supporting surface (22) are provided on the surface of the fibrous fabric (12) opposite to the dimensionally stable mold part (4) to inject the resin mixture and to ensure the connection with the pressure sink. The supporting surface (22) of the pipes has a narrow slit (26) which extends substantially over the whole length of the pipes and which is in communication over its whole length with the cavity (24). At least one end of the pipes extends outwards through the edges of the elastically deformable and dimensionally stable mold parts and is linked to the resin supply pipe or to the pressure sink. The mold (2) is evacuated down to an inner pressure of less than 50 hPa.
    • 在通过树脂传递模塑从纤维增强复合材料制造大表面结构元件的方法中,可以抽真空的模具(2)具有尺寸稳定的部分(4)和可弹性变形的部分(6)。 模具(2)具有用于注入树脂混合物和连接到压力罐的连接。 将纤维织物(12)放入模具(2)中。 在与尺寸稳定的模具相对的纤维织物(12)的表面上设置有具有大的支撑表面(22)和在支撑表面(22)上方的管道的纵向方向上延伸的空腔(24)的细长管 部分(4)注入树脂混合物并确保与压力池的连接。 管道的支撑表面(22)具有窄的狭缝(26),其基本上在整个管子的整个长度上延伸,并且其整个长度与空腔(24)连通。 管道的至少一端向外延伸穿过可弹性变形和尺寸稳定的模具部件的边缘,并且连接到树脂供应管或压力槽。 将模具(2)抽空至小于50hPa的内部压力。