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method of producing a rohrabschnitts a flugkörperaußenhülle and rohrabschnitt a flugkörperaußenhülle

机译:制造导弹外壳的管段的方法和导弹外壳的管段的制造方法

摘要

The new pipe section of a thermally highly loaded flight body the outside casing should be designed in such a way that the tube section over a longer period of time is to be able to withstand a high air friction. [0046] fig. 3 for this purpose, the new pipe section (1) the following features: a) of the pipe section (1) is formed by the fact that at least one prepreg (10) in overlapping layers (2) and wound up under a pressure and a temperature has been cured, b) the overlapping layers (2) are arranged like a cone stump jacket and based on the longitudinal direction by an angle of inclination (a) according to the front, c) of the angle of inclination (a) is 1° to 10°, d) the used prepreg (10) has a reinforced with fibers (11) matrix (12), e) the fibers of the prepreg tape (10) have a main orientation, f) the main alignment of the fibers (11) is in the transverse direction (q) of the prepreg tape (10).
机译:热负荷较高的飞行器外壳的新管段的设计应使管段在较长时间内能够承受高空气摩擦。 [0046]图。为此,如图3所示,新的管段(1)具有以下特征:a)管段(1)是通过以下事实形成的:至少一个预浸料(10)处于重叠的层(2)中并在压力下卷绕并已固化温度; b)重叠层(2)像圆锥形树桩套一样排列,并根据纵向方向按照与正面成一定角度的倾斜角(a)布置,c)倾斜角(a) )是1°到10°,d)用过的预浸料(10)用纤维(11)基质(12)增强,e)预浸料带(10)的纤维具有主要取向,f)主要排列纤维(11)的一部分在预浸料带(10)的横向方向(q)上。

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