| Literature DB >> 35310813 |
Patrick G Mongan1,2, Vedant Modi2, John W McLaughlin2, Eoin P Hinchy1,2, Ronan M O'Higgins2,3, Noel P O'Dowd1,2,3, Conor T McCarthy1,2,3.
Abstract
The use of composite materials is increasing in industry sectors such as renewable energy generation and storage, transport (including automotive, aerospace and agri-machinery) and construction. This is a result of the various advantages of composite materials over their monolithic counterparts, such as high strength-to-weight ratio, corrosion resistance, and superior fatigue performance. However, there is a lack of detailed knowledge in relation to fusion joining techniques for composite materials. In this work, ultrasonic welding is carried out on a carbon fibre/PEKK composite material bonded to carbon fibre/epoxy composite to investigate the influence of weld process parameters on the joint's lap shear strength (LSS), the process repeatability, and the process induced defects. A 33 parametric study is carried out and a robust machine learning model is developed using a hybrid genetic algorithm-artificial neural network (GA-ANN) trained on the experimental data. Bayesian optimisation is employed to determine the most suitable GA-ANN hyperparameters and the resulting GA-ANN surrogate model is exploited to optimise the welding process, where the process performance metrics are LSS, repeatability and joint visual quality. The prediction for the optimal LSS was subsequently validated through a further set of experiments, which resulted in a prediction error of just 3%.Entities:
Keywords: Artificial neural network; Bayesian optimisation; Dissimilar materials; Genetic algorithm; Machine learning; Ultrasonic welding
Year: 2022 PMID: 35310813 PMCID: PMC8924134 DOI: 10.1007/s10845-022-01911-6
Source DB: PubMed Journal: J Intell Manuf ISSN: 0956-5515 Impact factor: 6.485
Description of the laminates used during welding
| Material | Supplier | Stacking sequence | No. of plies | Matrix | Thickness (mm) |
|---|---|---|---|---|---|
| CF/PEKK | Teijin GmbH | 16 | Thermoplastic | 2.2 | |
| CF/Epoxy | Hexcel | 16 | Thermoset | 2.2 |
Fig. 1a Schematic of welding configuration and b welded specimen geometry.
Parameter and level combinations for the DoE
| Parameters | Level 1 | Level 2 | Level 3 |
|---|---|---|---|
| Welding energy (kJ) | 1.0 | 1.75 | 2.5 |
| Vibration amplitude (µm) | 85 | 100 | 115 |
| Welding force (N) | 400 | 800 | 1200 |
Experimental results with categorised defects and repeatability
| Physical run number | Welding energy (kJ) | Vibration amplitude (µm) | Welding force (N) | LSS (MPa) | RSD (%) [repeatability class] | Defect class |
|---|---|---|---|---|---|---|
| 29/30/69 | 1 | 85 | 400 | 12.90 | 24.41 [2] | 2 |
| 39/40/74 | 1 | 85 | 800 | 13.50 | 52.99 [3] | 2 |
| 25/26/67 | 1 | 85 | 1200 | 22.04 | 13.83 [2] | 1 |
| 37/38/73 | 1 | 100 | 400 | 10.79 | 54.87 [3] | 3 |
| 35/36/72 | 1 | 100 | 800 | 17.43 | 21.47 [2] | 1 |
| 21/22/65 | 1 | 100 | 1200 | 23.41 | 11.71 [2] | 2 |
| 45/46/77 | 1 | 115 | 400 | 14.48 | 8.35 [1] | 1 |
| 31/32/70 | 1 | 115 | 800 | 17.38 | 8.52 [1] | 1 |
| 49/50/79 | 1 | 115 | 1200 | 6.04 | 18.90 [2] | 1 |
| 21/52/80 | 1.75 | 85 | 400 | 22.26 | 9.98 [1] | 2 |
| 15/16/62 | 1.75 | 85 | 800 | 10.56 | 28.80 [2] | 2 |
| 19/20/64 | 1.75 | 85 | 1200 | 2.59 | 35.98 [3] | 3 |
| 9/10/59 | 1.75 | 100 | 400 | 16.38 | 13.15 [2] | 2 |
| 23/24/66 | 1.75 | 100 | 800 | 19.71 | 6.45 [1] | 2 |
| 3/4/56 | 1.75 | 100 | 1200 | 25.98 | 1.01 [1] | 3 |
| 41/42/75 | 1.75 | 115 | 400 | 17.12 | 25.31 [2] | 1 |
| 17/18/63 | 1.75 | 115 | 800 | 16.26 | 24.84 [2] | 2 |
| 11/12/60 | 1.75 | 115 | 1200 | 16.22 | 14.80 [2] | 1 |
| 7/8/58 | 2.5 | 85 | 400 | 15.48 | 24.95 [2] | 3 |
| 1/2/55 | 2.5 | 85 | 800 | 14.33 | 18.74 [2] | 1 |
| 47/48/78 | 2.5 | 85 | 1200 | 5.06 | 95.03 [3] | 3 |
| 43/44/76 | 2.5 | 100 | 400 | 9.70 | 25.50 [2] | 3 |
| 33/34/71 | 2.5 | 100 | 800 | 6.62 | 70.70 [3] | 3 |
| 53/54/81 | 2.5 | 100 | 1200 | 6.79 | 73.03 [3] | 3 |
| 13/14/61 | 2.5 | 115 | 400 | 11.59 | 78.05 [3] | 3 |
| 27/28/68 | 2.5 | 115 | 800 | 12.46 | 5.76 [1] | 3 |
| 5/6/57 | 2.5 | 115 | 1200 | 7.57 | 82.76 [3] | 2 |
Classification of process repeatability
| Class | RSD (%) |
|---|---|
| 1 | 0 < RSD ≤ 10 |
| 2 | 10 < RSD ≤ 30 |
| 3 | 30 < RSD |
Fig. 2Classification of joint quality based on visual assessment
Fig. 3Main effects plot and Pearson’s correlation coefficient (PCC) between input parameters and LSS
Fig. 4Surface plots displaying the results of the DoE, a distribution in LSS, b repeatability of the process and c the variation in defect class
Fig. 5Schematic displaying process flow for generating the supervised optimisation model
Hyperparameter bounds for BO
| Hyperparameter | Bound | Optimal |
|---|---|---|
| [1, 4] | 2 | |
| [4, 30] | 20, 20 | |
| α | [0.0001, 0.5] | 0.054 |
Hyperparameters values of the GA
| Hyperparameter | Value |
|---|---|
| Number of models | 12 |
| Number of mating parents | 8 |
| Mutation rate (%) | 10 |
| Generations | 2500 |
Fig. 6The optimised ANN configuration and the ANN process of prediction through a single compute neuron
Fig. 7Summary of predictions. a Regression analysis, b residual analysis
Fig. 8Joint before and after destructive testing produced under the predicted optimal input configuration
Comparison between the predicted and actual responses achieved under optimal conditions
| Output | Actual (all) | Actual (average ± SD) | Predicted | Accuracy (%) |
|---|---|---|---|---|
| LSS (MPa) | [24.11, 24.61, 24.65] | 24.5 ± 0.3 | 25.3 | 97 |
| Defect class (1–3) | [1, 1, 1] | 1 | 1 | 100 |
| Repeatability class (1–3) | [1, 1, 1] | 1 | 1 | 100 |