Title:
AIRCRAFT PANEL MANUFACTURING METHOD AND AIRCRAFT PANEL MANUFACTURING SYSTEM
Document Type and Number:
Japanese Patent JP2017136931
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide an aircraft panel manufacturing method and an aircraft panel manufacturing system capable of assembling aircraft panels with good accuracy.SOLUTION: An aircraft panel manufacturing method includes the steps of: causing a holding jig 1 to hold a fuselage panel 10 having a plurality of plate-like members having a cross section of a curve shape in such a manner that the cross section of the fuselage panel 10 becomes a curve shape protruding upward; overlapping the plurality of plate-like members of the fuselage panel 10 held by the holding jig 1 and connecting the overlapped portions by rivets; moving the holding jig 1 in which the fuselage panel 10 in which the plurality of plate-like members are connected are held; and connecting a frame 32 along the curve shape of the fuselage panel 10 by the rivets with respect to the plurality of plate-like members of the fuselage panels 10 held by the moved holding jig 1.SELECTED DRAWING: Figure 2
Inventors:
HIRAI MAKOTO
TANEDA YUJI
GOTO TAKUYA
KANEKO TAKESHI
TANEDA YUJI
GOTO TAKUYA
KANEKO TAKESHI
Application Number:
JP2016018428A
Publication Date:
August 10, 2017
Filing Date:
February 02, 2016
Export Citation:
Assignee:
MITSUBISHI HEAVY IND LTD
International Classes:
B64F5/00; B21J15/14; B64C1/12
Domestic Patent References:
| JP2015054324A | 2015-03-23 | |||
| JP2015030348A | 2015-02-16 | |||
| JP2013198918A | 2013-10-03 | |||
| JP2013124099A | 2013-06-24 |
Foreign References:
| EP0956915A2 | 1999-11-17 | |||
| US20130019446A1 | 2013-01-24 | |||
| US20120011693A1 | 2012-01-19 | |||
| US6121781A | 2000-09-19 | |||
| US5649888A | 1997-07-22 | |||
| EP2883797A1 | 2015-06-17 |
Attorney, Agent or Firm:
Noriharu Fujita
Miori Takao
Kawakami Miki
Takayuki Ishimoto
Daisuke Nagata
Miori Takao
Kawakami Miki
Takayuki Ishimoto
Daisuke Nagata