07-07-2023 дата публикации
Номер: CN116393971A
Автор:
LI CHANGJUN,
QIAN JUNJIE,
DONG ZIRUI,
YAN GUANJUN,
LI SHUYANG,
ZHONG HANTIAN,
CHEN HONG,
WANG DONGLIANG,
MIAO XINCONG,
JIANG QIANG,
JI CHUANG
Принадлежит:
The invention provides a flexible satellite mounting method for a solar wing in a folded state. The method comprises the following steps: a, fixedly connecting the upper sides of an inner plate, a middle plate and an outer plate of the solar wing by using an upper fixing tool; b, fixedly connecting the lower sides of the inner plate, the middle plate and the outer plate of the solar wing by using a lower fixing tool; c, a connecting frame of the solar wing, the inner plate, the middle plate and the left side of the outer plate are fixedly connected through a left fixing tool; d, a right fixing tool is used for fixedly connecting the connecting frame, the inner plate, the middle plate and the right side of the outer plate of the solar wing; e, a root hinge of the solar wing is connected with the left fixing tool through a root fixing tool; f, connecting and fixing the upper, lower, left and right fixing tools by using an integral fixing tool; g, the solar wing and tool combination body is ...
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