22-07-2009 дата публикации
Номер: CN0101486144A
Автор:
FENG ZIMING,
DU BAORUI,
SUN JINPING,
OU YANG,
DENG HAIZHOU,
SONG BAOWEI,
ZHENG WEIDONG,
CAO XINHUA,
HUANG NING,
ZIMING FENG,
BAORUI DU,
JINPING SUN,
YANG OU,
HAIZHOU DENG,
BAOWEI SONG,
WEIDONG ZHENG,
XINHUA CAO,
NING HUANG
Принадлежит:
The invention relates to a flexible assembly frock, which is a frock for assembling structural parts of an aircraft. The flexible assembly frock is characterized by consisting of a spliced assembly frame, a driving and revolving mechanism, automatic drilling equipment and a pneumatic positioning and clamping mechanism, wherein the spliced assembly frame is arranged on the driving and revolving mechanism; the automatic drilling equipment is arranged on the ground; the pneumatic positioning and clamping mechanism is arranged on both sides of the spliced assembly frame; the spliced assembly frame consists of long-slot three-dimensional profile steels, 45 DEG slotted three-dimensional profile steels, short-slot three-dimensional profile steels, a positioner, a pneumatic clamper, a clamping plate, chute three-dimensional profile steels, a positioning shaft and hand wheels; the driving and revolving mechanism consists of a baffle plate, a bearing I, a base, a bearing II, a rotating shaft, a connecting ...
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