| 某型飞机机身合拢总装型架设计新技术 |
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| 引用本文： | 王文江.某型飞机机身合拢总装型架设计新技术[J].洪都科技,2003(1):6-8. |
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| 作者姓名： | 王文江 |
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| 作者单位： | 洪都航空工业集团工装设计所 |
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| 摘 要： | 某型飞机机身合拢总装型架，在设计上采用了先进制造技术。型架上装有目前国际先进的光学坐标系统，型架地基采用整体框架式底盘。型架结构为分散式。按飞机飞行状态在型架中摆放，并由上方起吊形式下架。本文简要介绍了该型架的设计、制造情况及效果。
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| 关 键 词： | 飞机 总装 机身 飞行状态 合拢 架设 底盘 新技术 坐标系统 地基 |
| 修稿时间： | 2002年9月10日 |
NEW TECHOLOGY FOR DESIGN OF SOME- MODEL A/C FUSELAGE BUTT -JOINT FINAL ASSEMBLY JIG |
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| Wang wenjiang.NEW TECHOLOGY FOR DESIGN OF SOME- MODEL A/C FUSELAGE BUTT -JOINT FINAL ASSEMBLY JIG[J].Hongdu Science and Technology,2003(1):6-8. |
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| Authors: | Wang wenjiang |
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| Institution: | Tooling Design Institute of Hongdu Aviation Industry Group |
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| Abstract: | The aircraft fuselage butt-joinging final-assembly jig used for some model of aircraft adopts the advanced fabrication technology in design.The advanced optical coordinate system currently used in the world has been fitted on the jig.The jig foundation is to adopt the integral frame bottom.The jig is a separated structure,which is located in the jig according to the aircaraft flight attitude,and settled down by hoist from above.This paper is to briefly introduce the jig design and fabrication as well as its effectiveness. |
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| Keywords: | Fuselage butt-joint Final-assembly Jig Optical coordinate system Foundation Frame |
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