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Aircraft fuselage assembly system and assembly method

An assembly system and aircraft fuselage technology, applied in aircraft assembly and other directions, can solve the problems of low assembly quality and low assembly efficiency, and achieve the effects of improving assembly quality, efficiency, and production continuity

Pending Publication Date: 2022-04-05
CHENGDU AIRCRAFT INDUSTRY GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The main purpose of this application is to provide an aircraft fuselage assembly system and assembly method, aiming to solve the technical problems of low assembly efficiency and low assembly quality in existing aircraft component assembly methods

Method used

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  • Aircraft fuselage assembly system and assembly method
  • Aircraft fuselage assembly system and assembly method
  • Aircraft fuselage assembly system and assembly method

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Embodiment 1

[0055] refer to Figure 1-Figure 17 , the present embodiment provides an aircraft fuselage assembly system and assembly method, including an assembly platform 100, an assembly tool 200, a positioning workbench 300, a processing machine tool 400 and an AGV trolley 500, the assembly platform 100 is used to carry staff, and the assembly tool 200 Located in the assembly platform 100, the assembly tooling 200 is used to assemble aircraft components, the positioning workbench 300 is used to clamp the assembled aircraft components, the processing machine tool 400 is used to perform drilling and riveting on the assembled aircraft components, and the AGV trolley 500 is used to Transport aircraft parts.

[0056] In this embodiment, the aircraft parts can be assembled with the help of the assembly platform 100 and the assembly tool 200. The assembly platform 100 can complete the assembly work of different heights of the large aircraft parts. At the same time, the aircraft components are...

Embodiment 2

[0083] refer to Figure 1-Figure 18 , the present embodiment provides an assembly method based on the aircraft fuselage assembly system described in Embodiment 1, comprising the following steps:

[0084] The components are transported to the assembly platform 100 by the AGV trolley 500;

[0085] Assemble the aircraft components through the assembly tooling 200 in the assembly platform 100;

[0086] Transport the assembled aircraft components to the positioning workbench 300 through the AGV trolley 500;

[0087] Install the assembled aircraft parts on the positioning workbench 300;

[0088] The positioning workbench 300 equipped with aircraft parts is transported to the processing machine tool 400 as a whole through the AGV trolley 500;

[0089] The assembled aircraft components are drilled and riveted by the processing machine tool 400 .

[0090] In this embodiment, the aircraft parts are assembled with the help of the assembly platform 100 and the assembly tool 200. The a...

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Abstract

The invention discloses an aircraft fuselage assembling system and method, the system comprises an assembling platform, an assembling tool, a positioning workbench, a machining tool and an AGV trolley, the assembling platform is used for bearing workers, the assembling tool is located in the assembling platform and used for assembling aircraft parts, the positioning workbench is used for clamping the assembled aircraft parts, and the machining tool is located in the assembling platform and used for clamping the assembled aircraft parts; the machine tool is used for drilling and riveting the assembled aircraft parts, the AGV is used for transporting the aircraft parts, and the aircraft part assembling device has the advantages of being high in assembling quality and high in assembling efficiency.

Description

technical field [0001] The present application relates to the technical field of aircraft assembly, in particular to an aircraft fuselage assembly system and assembly method. Background technique [0002] At present, in view of the bottleneck problem of aircraft digital assembly and processing technology, which restricts the improvement of aircraft development and production capacity of my country's aviation manufacturing enterprises, the structure of the aircraft body is complex, and the number of parts and connectors is large. A large aircraft has nearly 100,000 parts. More than 1 million rivets; during the aircraft assembly process, a large number of aircraft parts are gradually assembled into assemblies, panels, segments and parts in a certain combination and order, and finally the parts are butted into a complete aircraft body. The large parts of the fuselage require long life, high strength, sealing, and fatigue resistance, and have very high requirements for the prepar...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/10
Inventor 赵茜孙海龙雷沛曾超陈强代玉淋云鑫庞大伟田家强揭璐瑞
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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