Error Analysis Model of Aircraft Multi-Joint Assembly Based on Linkage Mechanism Theory
Keyword(s):
Multi-joint link is a class of typical structure in aircraft assembly. And the quantification of assembly error is very important to tolerance allocation and assembly quality prediction. A novel error analysis model of multi-joint assembly is established based on linkage mechanism theory. First, a virtual linkage mechanism will be created according to specific structural character and tolerance of joint linkage. And then, the input-output equation of linkage mechanism can be derived by vector method. Subsequently, the coaxiality and coplanarity error analysis models are developed respectively for three-joint and four-joint assembly. Finally, a case study on the elevator & horizontal empennage docking demonstrates the proposed method.
Keyword(s):
2021 ◽
Vol ahead-of-print
(ahead-of-print)
◽
Keyword(s):
Keyword(s):
2019 ◽
Vol 233
(17)
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pp. 6005-6025
Keyword(s):
2014 ◽
Vol 602-605
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pp. 779-782
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