The purpose of this work is to demonstrate the application of a robust design procedure to the design of aircraft structures. Taguchi's method of robust design has been applied to obtain the most appropriate values of a set of control factors considering several noise factors. The goal is to maximize the robustness of the design and decrease the loss of quality. A description of the methodology is provided and an application example is solved, using a selected set of noise and control factors, to describe the suitability of this technique for structural design in problems where inaccuracies are present. The results show an improvement in the response of the components, maintaining a low dependence on input value variations and producing designs that increase the quality level and enhance the robustness. Other different sets can be defined, as the method is completely general.
An application of Taguchi's method to robust design of aircraft structures
Die Anwendung der Taguchi-Methode für die Entwicklung stabiler Luftfahrtstrukturen
2012
10 Seiten, 4 Bilder, 7 Tabellen, 5 Quellen
Conference paper
English
Robust Design for Occupant Protection System Using Taguchi's Method
British Library Conference Proceedings | 2007
|Robust Design for Occupant Protection System Using Taguchi's Method
SAE Technical Papers | 2007
|Daily Peak Load Forecasting by Taguchi's T Method
Online Contents | 2017
|Gear Noise Development Using Dr. Taguchi's Tolerance Design of Experiment Approach
SAE Technical Papers | 1992
|