High-precision flexible coordination assembly method for functional components of carrier rocket cabin section

The invention provides a carrier rocket cabin functional assembly high-precision flexible coordination assembly method. The method comprises the following steps that S1, the installation positions of a laser projector and a laser tracker are determined; s2, establishing a measurement coordinate syst...

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Hauptverfasser: SUN JIANLI, LIU SHAORUI, LIU YANPING, GUO ZHEN, YANG SHUAI, QIAO GUOHUA, PENG JIANGTAO, WU LINXUAN, QIAN WEI, WAN SHUHUI, MA GUOYE, JIA XIAOFEI, HAN JIN, SHEN LINYUAN, MU JING, LYU XIAOMIN, ZHANG XIAOFANG, WANG JIANGANG
Format: Patent
Sprache:chi ; eng
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Zusammenfassung:The invention provides a carrier rocket cabin functional assembly high-precision flexible coordination assembly method. The method comprises the following steps that S1, the installation positions of a laser projector and a laser tracker are determined; s2, establishing a measurement coordinate system; s3, establishing a process model composed of a separation spring support, a guide ring, a front end frame, a rear end frame, a stringer and an explosive bolt box by using three-dimensional modeling software; s4, selecting a positioning reference in the process model created in the step S3; s5, the contour lines of the release spring support and the guide ring are projected to the outer surface of the cabin section through a laser projector for coarse positioning; S6, the guide ring is positioned through an auxiliary tool under the frame; and S7, the laser tracker is used for measuring and aligning the accurate positions of the separation spring support and the guide ring. Dependence of products on tools is redu