A circular numerical control automatic hole-making system for aircraft fuselage docking assembly

An aircraft fuselage, automatic manufacturing technology, applied in aircraft parts, manufacturing tools, transportation and packaging, etc., can solve the problems of frequent tool change processing efficiency, large axial force of hole making, etc., to improve the flexibility of hole making, improve the Efficiency, the effect of enhancing precision

Active Publication Date: 2017-08-29
NANJING COLLEGE OF INFORMATION TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved by the present invention is that existing aircraft fuselage docking automatic drilling systems have problems such as large hole-making axial force, frequent tool changes for different hole diameters, and low processing efficiency.

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  • A circular numerical control automatic hole-making system for aircraft fuselage docking assembly
  • A circular numerical control automatic hole-making system for aircraft fuselage docking assembly
  • A circular numerical control automatic hole-making system for aircraft fuselage docking assembly

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Embodiment Construction

[0030] like figure 1 As shown, the present invention is used for the circular numerical control automatic hole-making system of aircraft fuselage butt joint assembly and comprises: two circular track assemblies 1000, four four-wheel drive carrying devices 2000 that move along two circular track assemblies 1000 and be installed on four-wheel drive carrying The automatic hole making device 3000 on the device 2000.

[0031] like figure 2 and 3 As shown, the circular track assembly 1000 includes a flexible track module 1100 and a vacuum chuck assembly 1200, wherein each circular track assembly 1000 may include several flexible track modules 1100; each flexible track module 1100 includes a flexible track support 1101, two guide slides Groove 1102 and arc-shaped flexible rack 1103; two guide chute 1102 are respectively installed on both sides of the flexible track support 1101, and the arc-shaped flexible rack 1103 is arranged on the track outer ring of the flexible track support...

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Abstract

The invention provides an annular numerical control automatic hole manufacturing system used for butt joint assembly of an airplane body. The annular numerical control automatic hole manufacturing system comprises two annular rail assemblies, at least two four-drive carrying devices moving along the two annular rail assemblies, and automatic hole manufacturing devices installed on the four-drive carrying devices. Each annular guide rail assembly comprises a flexible rail module and a vacuum sucker assembly. Each four-drive carrying device comprises a first double-drive electric control trolley and a second double-drive electric control trolley. Each automatic hole manufacturing device comprises a normal posture adjusting mechanism, a drilling and milling hole manufacturing unit and a pressing and chip removing mechanism. By means of the annular numerical control automatic hole manufacturing system, due to the fact that a certain number of the automatic hole manufacturing devices and a certain number of the four-drive carrying devices are reasonably arranged, the overall rigidity of the annular rail assemblies can be enhanced, and therefore the machining quality of holes is ensured, and the hole machining efficiency can also be obviously improved.

Description

technical field [0001] The invention relates to a numerically controlled automatic hole-making system, in particular to a ring-shaped automatic hole-making system for fuselage docking assembly, belonging to the field of automatic hole-making for aircraft digital assembly. Background technique [0002] The quality and efficiency of the fuselage docking assembly holes directly restrict the assembly cycle, manufacturing cost and safety performance of the whole machine, and have always been a research hotspot in aircraft digital assembly. In this regard, foreign countries took the lead in proposing a flexible track hole-making system. Therefore, the equipment has a high degree of automation, flexibility and convenience, and can complete the functions of drilling and countersinking at one time, but the overall rigidity of the system is poor, and the processing stability is insufficient. In order to solve the above problems, Chinese invention 201410123510.8 proposes a system and ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23P23/02
CPCB23P23/02B23P2700/01
Inventor 单以才章婷刘世豪舒平生颜玮
Owner NANJING COLLEGE OF INFORMATION TECH
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