Uncertainty Modeling for Aircraft Interior Noise - Composites Transmission Loss Optimization

摘要

Although the aerospace production process is much better controlled than the process in other industries, it remains true that very small manufacturing variability exists in the geometrical parameters (flange thicknesses, hole diameters …) as well as in material properties.). Also the medical, nuclear, and even the toy industry manufacturers assemble their products to very controlled and tight tolerances, thus receiving the always more stringent quality requirements imposed by customers, regulations and safety. However, despite this clear trend towards improved quality in products, in the current design process, the effect of this manufacturing variability is usually compensated for by applying safety factors. This is not an ideal situation, as it may lead to slightly over-designed structures. A much more promising approach is to include probabilistic models of design variables into the mechanical simulation process. This approach has been investigated first for space structures and construction industry and has now reached a sufficient maturity level to become an integral part of the product design process in industry, especially in those fields - like aeronautics - where safety is a critical requirement of every airborne structure. Then, with a new methodology based on reliability analysis, engineers can obtain a better understanding of the actual effect of the manufacturing tolerances and of variability in material properties. Based on the analysis results, the robustness and reliability of the design can be assessed and improved if needed. In this paper, the above-mentioned probabilistic approach is applied for the analysis of a stiffened composite panel of an aircraft and its acoustic performances in terms of transmission loss. The frequency dependent transmission loss of this composite structure is optimized with respect to two ply thicknesses and four material properties in order to obtain a high transmission loss throughout different frequencies for good acoustic insulation. The objective of this study is to maximize the minimum transmission loss throughout the entire acoustic frequency spectrum. The structural behavior of the composite panel is calculated with the Finite Element Method, while the acoustic performance is predicted with the Boundary Element method. The combination of both modeling techniques allows accurate prediction of the panel's transmission loss. During the optimization process, the parameters are initially optimized using deterministic approaches: first a global search is used, followed by a refinement procedure that uses a local search algorithm. This first optimization does not take into consideration any parameter variability. The solution found by the deterministic approaches is then used as the starting point for the probabilistic approach to improve the reliability and robustness. For this purpose, the Performance Measure Approach (that uses the inverse reliability problem formulation) has been used to perform a robustness based design optimization (RBDO) process. The two optimization approaches use surrogate models constructed on the results of a Design of Experiments in order to save computational time. In this way, optimal solutions were obtained with a fraction of the otherwise required number of mechanical simulation runs. The deterministic approaches improved the transmission loss from 8.8 dB of the reference configuration to 13.6 dB.