AIRCRAFT COMPONENT ASSEMBLY JIG, AND AIRCRAFT COMPONENT INSPECTION JIG

WIPO Patent Application WO/2020/045649

A1

An aircraft component assembly jig (10A) is provided with: a plurality of header plates (12); receiving members (13), a plurality of which are provided on each header plate (12), and distal ends of which abut an upper surface or a lower surface of an aircraft component; receiving member moving units (14) which move the receiving members (13) forward and backward; receiving member state detecting units (30) which detect, as control data, a support state of the lower surface of the aircraft component by each receiving member (13); and a control unit (20A). The control unit (20A) compares a detected value of the detected control data with a predetermined reference value, to determine whether a uniform support state of the aircraft component by all the receiving members (13) has been achieved. Then, if it is determined that a uniform support state has not been achieved, the receiving member moving units (14) for which adjustment is required, among all the receiving member moving units (14), are controlled to adjust the forward/backward position of each receiving member (13) within a drawing tolerance.

JP2009028818

ROBOT SYSTEM

OKADA HIDEKI
MATSUI SHUJI
YANO FUMINORI
KASAHARA KENJI

PCT/JP2019/034211

March 05, 2020

August 30, 2019

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KAWASAKI HEAVY IND LTD (JP)

B23P19/00; B64F5/10; B23P21/00; B64C1/06

JP2017193241A	2017-10-26
JP2017193242A	2017-10-26
US20130040008A1	2013-02-14
JP2012213836A	2012-11-08
JP2013198918A	2013-10-03
JP2008169038A	2008-07-24

PATENT CORPORATE BODY ARCO PATENT OFFICE (JP)

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