DocumentCode
569701
Title
A design of aircraft drilling end-effector based on flexible railway
Author
Ma, Fucun ; Yuan, Peijiang ; Gong, Maozhen ; Yu, Leibin ; Xing, Hongwen ; Huang, Wen
Author_Institution
Sch. of Mech. Eng. & Autom., BUAA, Beijing, China
fYear
2012
fDate
25-27 July 2012
Firstpage
536
Lastpage
539
Abstract
This paper describe a design of aircraft drilling end-effector (ADEE) based on flexible railway which is mainly used for drilling on the surface of fuselage and wing of aircraft. The whole system is composed of several different modules. Flexible railway module (FRM) make ADEE move to any places where need to be drilled. Framework and Z axis module (FZM) uses high-rigidity framework and linear slide guide to guarantee the precision and stability of the drilling action. Compression and absorbing chipping module (CACM) adopts symmetric double-cylinder structure and generates 1000N compressing forces that can compress three layers aircraft skin and is increased by demand. Vacuous absorbing chipping mechanism uses high flow vacuum generator as vacuum air source and filters metal shavings by filter. Visual inspection module (VIM) can precisely calculate the distance between three points around drill bit and finished surface by calculating, and then achieves verticality deviation value through normal detection algorithm. Binary angular adjustment module (BAAM) revises angle deviation that is caused by the differences of adsorption position diameter of two rows of rack. ADEE is more flexible and better adaptable; meanwhile, it can greatly improve the efficiency and precision of the holes. It does not use drilling fluids in the whole manufacturing process and fundamentally eliminates the pollution problem of the drilling fluid. In conclusion, experiments show that ADEE can meet the requirements of automatic drilling of departments of aircraft and greatly enhance the quality and speed of drilling holes.
Keywords
aerospace components; drilling; end effectors; inspection; robotic assembly; ADEE; BAAM; CACM; FRM; FZM; VIM; absorbing chipping mechanism; adsorption position diameter; aircraft drilling end-effector; aircraft fuselage; aircraft wing; binary angular adjustment module; compressing forces; compression-and-absorbing chipping module; drilling fluid; flexible railway module; framework-and-Z axis module; high flow vacuum generator; high-rigidity framework; linear slide guide; normal detection algorithm; symmetric double-cylinder structure; visual inspection module; Aircraft; Aircraft manufacture; Assembly; Drilling machines; Manuals; Rail transportation; Robots; aircraft drilling end-effector; binary angular adjustment mechanism; bionics; flexible railway;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Informatics (INDIN), 2012 10th IEEE International Conference on
Conference_Location
Beijing
Print_ISBN
978-1-4673-0312-5
Type
conf
DOI
10.1109/INDIN.2012.6301232
Filename
6301232
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