2018
DOI: 10.1007/s00170-018-2048-0
|View full text |Cite
|
Sign up to set email alerts
|

Working mode in aircraft manufacturing based on digital coordination model

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
10
0
1

Year Published

2019
2019
2022
2022

Publication Types

Select...
5
2

Relationship

1
6

Authors

Journals

citations
Cited by 40 publications
(12 citation statements)
references
References 29 publications
0
10
0
1
Order By: Relevance
“…From Table 1, it can be concluded that most research focuses on turbines [24][25][26][27][28][29][30][31][32][33][34][35][36][37] and aeroengines [14,[45][46][47][48][49][50][51][52]. In terms of the application of turbines, research on wind turbines [30][31][32][33][34][35][36][37] accounts for a large proportion.…”
Section: Overview On Life Cycle Of Turbomachinery With Digital Twinmentioning
confidence: 99%
See 2 more Smart Citations
“…From Table 1, it can be concluded that most research focuses on turbines [24][25][26][27][28][29][30][31][32][33][34][35][36][37] and aeroengines [14,[45][46][47][48][49][50][51][52]. In terms of the application of turbines, research on wind turbines [30][31][32][33][34][35][36][37] accounts for a large proportion.…”
Section: Overview On Life Cycle Of Turbomachinery With Digital Twinmentioning
confidence: 99%
“…In terms of the application of turbines, research on wind turbines [30][31][32][33][34][35][36][37] accounts for a large proportion. In the aerospace field, some scholars have made efforts on aeroengines [45,47], while others have studied aircraft [14,[49][50][51][52].…”
Section: Overview On Life Cycle Of Turbomachinery With Digital Twinmentioning
confidence: 99%
See 1 more Smart Citation
“…With the concept of importance degree [34], it can be taken as the affected degree. Then the quality loss of the whole coordination features  …”
Section: A Identification Of the Pcfmentioning
confidence: 99%
“…The main parts are separated as ribs, spar(s), hinge joints, skin panel etc., as shown in Figure 13. The two components would be joined together at the interface of 14 th rib and the 15 th rib to be a complete component [34]. On the macroscopic, the position and number of ribs that distributing on the spar are different from the inner one and the outer one.…”
Section: A Structure Of the Experimental Objectmentioning
confidence: 99%