Single step shimming solution for automated aircraft assembly-Reference-Cited by-同舟云学术

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Single step shimming solution for automated aircraft assembly

Published:2017-08 Issue: Volume: Page:
ISSN:
Container-title:2017 13th IEEE Conference on Automation Science and Engineering (CASE)
language:
Short-container-title:

Author:

Ehmke Fabian¹,Rao Sarvesh¹,Wollnack Jorg²

Affiliation:

1. Fraunhofer Institute for Manufacturing Technology and Advanced Materials IFAM, Ottenbecker Damm 12, 21684 Stade, Germany

2. Institute of Production Management and Technology, Hamburg University of Technology Denickestrasse 15 (K), 21073 Hamburg, Germany

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/8244402/8256062/08256179.pdf?arnumber=8256179

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effect of forced assembly on bearing performance of single-lap, countersunk composite bolted joints – Part Ⅱ: Numerical investigation;Composite Structures;2023-09

2. A pre-assembly analysis technology of aircraft components based on measured data;Measurement Science and Technology;2022-04-06

3. A multimodal optical approach for investigating 3D-printed carbon PEEK composites;Optics and Lasers in Engineering;2022-04

4. Gap volume prediction for aircraft wing assembly;Procedia Manufacturing;2021

5. Effect of Gap and Shims on the Strain and Stress State of the Composite-Aluminum Hybrid Bolted Structure;International Journal of Aerospace Engineering;2020-12-08

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