The embodiment of the invention provides a manufacturing method of an aerospace craft cabin section and the aerospace craft cabin section. The method comprises the following steps that structural design is conducted on the cabin section, and the structural design comprises a plurality of structural design steps; each structural design step corresponds to one process design and production step so as to manufacture a corresponding structure; and wherein all the process design and production steps and all the structural design steps are partially carried out in parallel. The aerospace craft cabinsection is manufactured through the manufacturing method of the aerospace craft cabin section. According to the embodiments of the manufacturing method of the aerospace craft cabin section and the aerospace craft cabin section, the technical problem that the manufacturing period of the aerospace craft cabin section is relatively long is solved.

    本申请实施例提供了一种航天飞行器舱段的制造方法及航天飞行器舱段。包括如下步骤:对舱段进行结构设计,所述结构设计包括多个结构设计步骤;每个所述结构设计步骤对应一个工艺设计及生产步骤,以制造出对应的结构;其中,各个所述工艺设计及生产步骤和各个所述结构设计步骤有部分是并行进行的。航天飞行器舱段通过上述航天飞行器舱段的制造方法制造得到。本申请实施例解决了航天飞行器舱段的制造周期较长的技术问题。


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    Title :

    Manufacturing method of aerospace craft cabin section and aerospace craft cabin section


    Additional title:

    航天飞行器舱段的制造方法及航天飞行器舱段


    Contributors:
    DING GUOYUAN (author) / SHAN YIJIAO (author) / FAN XINZHONG (author) / WANG NING (author) / CHEN ZENGKUI (author) / FANG ZEPING (author) / ZHANG JINYU (author) / LIANG ZUDIAN (author) / YANG DONGSHENG (author) / NIU FEI (author)

    Publication date :

    2021-02-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen / B64G Raumfahrt , COSMONAUTICS



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