Mold for molding a sleeve-equipped reinforced plastic tubular body, and method for handling the mold
    61.
    发明公开
    Mold for molding a sleeve-equipped reinforced plastic tubular body, and method for handling the mold 失效
    模具与用于处理模具由增强塑料制成,和方法的套筒管。

    公开(公告)号:EP0038555A1

    公开(公告)日:1981-10-28

    申请号:EP81103015.4

    申请日:1981-04-21

    IPC分类号: B29D3/02 B29D23/00 B29C1/00

    摘要: This invention relates to a method for molding a sleeve-type reinforced plastic tubular body, such as a pipe coupling, and to a mold therefor. According to the method of this invention, a sleeve-fitted reinforced plastic tubular body is produced by using a mold obtained by assembling a main body and sleeve-molding members fixable and axially slidable to and along the outside surface of the main body. Accordingly, by providing sleeve molding members of different configurations and sizes and using them exchangeably according to the configuration and size of the desired molded article, tubular bodies having a sleeve of different configurations and sizes can be molded as required. Furthermore by adjusting the fixing position of the sleeve-molding member with regard to the main body of the mold, tubular bodies having a tubular section of different lengths can be produced by using one type of mold.

    摘要翻译: 本发明涉及一种用于模制的套筒型增强塑料管状体,颜色:如管接头,以及一个模具为此。 。根据本发明,嵌合增强塑料管状体是通过使用通过组装主体和套筒模制构件可固定并轴向可滑动并沿主体的外表面而得到的模具制造的套筒的方法。 因此,通过提供不同的构型和尺寸的套筒模构件以及使用它们可交换gemäß到所需模塑制品的形状和尺寸,可以根据需要模制具有歧构型和尺寸的套筒的管状体。 进一步通过调整套筒模制构件的固定位置相对于所述模具的主体,可以通过使用一种类型的模具来生产具有不同长度的管状部分的管状体。

    Method of manufacturing tubes for lighting poles and the like
    62.
    发明公开
    Method of manufacturing tubes for lighting poles and the like 失效
    Verfahren zur Herstellung vonRöhrenfürLichtmasten und dgl。

    公开(公告)号:EP0014186A1

    公开(公告)日:1980-08-06

    申请号:EP80850009.4

    申请日:1980-01-23

    申请人: Omre, Torleif

    发明人: Omre, Torleif

    IPC分类号: B29D23/12 F21V21/10

    摘要: To make plastic tubes for lighting poles and the like, a core which is subdivided into a plurality of elements is utilized. The outer circumference of the combined elements corresponds to the desired tube circumference. A web of polyester/glass fiber is first wound around each element, after which the elements are fitted together and additional layers of the web are wound around the outer circumference of the composite unit. Extra reinforcing members may optionally be introduced. After curing, the core elements are removed.

    摘要翻译: 为了制造用于照明灯杆等的塑料管,使用细分为多个元件的芯。 组合元件的外圆周对应于所需的管圆周。 聚酯/玻璃纤维网首先缠绕在每个元件周围,之后将元件装配在一起,并且幅材的附加层缠绕在复合单元的外圆周上。 可以任选地引入额外的加强构件。 固化后,除去核心元素。

    TAPES
    64.
    发明公开
    TAPES 审中-公开

    公开(公告)号:EP3390015A1

    公开(公告)日:2018-10-24

    申请号:EP16805431.0

    申请日:2016-12-02

    IPC分类号: B29C70/16 B29C53/58

    摘要: The invention relates to a tape, comprising at least one layer comprising a. endless fiber in an total amount of at least 40 volume % as compared to the total volume of the layer and b. a thermoplastic matrix comprising one or more polyamides containing one or more aliphatic monomeric units, c. and optionally heat stabilizer, flame retardant, colorant, lubricant, mold release agent, UV stabilizer, impact modifier, laser absorbing additive as well as combinations thereof; wherein the one or more polyamides have a CH2-ratio of at least 5.5 and less than 10, calculated by - identifying the number of different aliphatic monomeric units in the one or more polyamides; - determining the number of CH2 groups per aliphatic monomeric unit for each of these different aliphatic monomeric units; - calculating the sum of the so determined numbers of CH2 groups; - dividing said sum by the number of different aliphatic monomeric units in the one or more polyamides; taking into account only the aliphatic monomeric units present in the one or more polyamides in an amount of at least 10 wt% with respect to the total weight of the one or more polyamides. The invention also relates to a vessel prepared by employing these tapes.

    Device for producing an airplane fuselage comprising an actuating system of sectors
    67.
    发明授权
    Device for producing an airplane fuselage comprising an actuating system of sectors 有权
    用于制造飞机机身,其包括扇区的致动系统的装置

    公开(公告)号:EP2644940B1

    公开(公告)日:2015-07-22

    申请号:EP13161888.6

    申请日:2013-03-29

    摘要: An actuating system of sectors of a device (2) for producing an airplane fuselage. Each sector is provided with an actuating system (27) of the screw - nut screw type in which a threaded element (31) is rotated about a rotation axis (32) by a motor (28). The threaded element (31) comprises an internal shaft (33) made of a first material and extending along the rotation axis (32) and an external tubular portion (34) made of a second material, mounted axially on a portion of the shaft and provided externally with a thread. Constraint means (38) are provided between the internal shaft (33) and the tubular portion (34) adapted to prevent angular displacement of the tubular portion (34) with respect to the internal shaft (33) allowing linear sliding of the tubular portion (34) with respect to the internal shaft (33). A thermal stress applied to the threaded element (31) produces the sliding of a free end portion (34a) of the tubular portion (34) with respect to the internal shaft (33) so that an increase in the temperature does not produce an overall elongation of the threaded element (31) maintaining each sector in the expanded lamination position previously defined.

    摘要翻译: 在用于制造飞机机身致动装置(2)的扇区的系统。 在哪一个螺纹元件(31)绕旋转轴线(32)由马达(28)的螺母螺杆式 - 每个扇区在螺杆致动系统(27)设置有。 所述螺纹元件(31)包括轴内部(33)由第一材料制成的,并沿所述旋转轴线(32),并在由第二材料制成的外部管状部分(34)延伸的轴向安装在轴的一部分和 具有螺纹外部提供。 内轴(33)和允许线性管状部分的滑动筒部(34)angepasst以防止所述管状部分(34)的角位移相对于所述内轴(33)(之间设置约束装置(38) 34)相对于所述内轴(33)。 施加到所述螺纹元件(31)的热应力使筒状部(34)的自由端部(34A)的滑动相对于所述内轴(33),以便确实在温度升高不会产生对总体 保持在扩张位置层压各扇区的螺纹元件(31)的伸长先前所定义。

    Actuating system of sectors of a device for producing an airplane fuselage
    70.
    发明公开
    Actuating system of sectors of a device for producing an airplane fuselage 有权
    用于制造飞机机身,其包括扇区的致动系统的装置

    公开(公告)号:EP2644940A1

    公开(公告)日:2013-10-02

    申请号:EP13161888.6

    申请日:2013-03-29

    摘要: An actuating system of sectors of a device (2) for producing an airplane fuselage. Each sector is provided with an actuating system (27) of the screw - nut screw type in which a threaded element (31) is rotated about a rotation axis (32) by a motor (28). The threaded element (31) comprises an internal shaft (33) made of a first material and extending along the rotation axis (32) and an external tubular portion (34) made of a second material, mounted axially on a portion of the shaft and provided externally with a thread. Constraint means (38) are provided between the internal shaft (33) and the tubular portion (34) adapted to prevent angular displacement of the tubular portion (34) with respect to the internal shaft (33) allowing linear sliding of the tubular portion (34) with respect to the internal shaft (33). A thermal stress applied to the threaded element (31) produces the sliding of a free end portion (34a) of the tubular portion (34) with respect to the internal shaft (33) so that an increase in the temperature does not produce an overall elongation of the threaded element (31) maintaining each sector in the expanded lamination position previously defined.