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The VITAL (EnVIronmenTALly Friendly Aero Engines) project funded by the European Commission under Framework 6 aims to provide significant reductions in aero-engine fuel burn, noise and emissions through the development of innovative design and manufacturing techniques. One method of reducing the amount of fuel burnt, and hence CO2 produced, is to reduce the weight of the engine. A significant proportion of an engine's weight is due to the large castings used to form the main non-rotating structures; the replacement of these with fabricated structures could provide a significant weight reduction. This paper describes the design and implementation of a robotic assembly cell for complex aero-engine components. A series of experiments were performed to prove the feasibility of the automated assembly process. The results presented indicate that automated robotic assembly is feasible and cost effective.
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5--16
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Bibliogr. 12 poz., tab., rys.
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- Mechanics, Materials & Structures Division and Manufacturing Division, Faculty of Engineering, University of Nottingham, University Park, Nottingham, NG7 2RD, UK
autor
- Mechanics, Materials & Structures Division and Manufacturing Division, Faculty of Engineering, University of Nottingham, University Park, Nottingham, NG7 2RD, UK
autor
- Mechanics, Materials & Structures Division and Manufacturing Division, Faculty of Engineering, University of Nottingham, University Park, Nottingham, NG7 2RD, UK
autor
- Mechanics, Materials & Structures Division and Manufacturing Division, Faculty of Engineering, University of Nottingham, University Park, Nottingham, NG7 2RD, UK
Bibliografia
- [1] ANDERSON J., Advanced Robotic Applications in Aircraft Component Assembly, Proceeding of Mechatronics, University of Twente, Netherlands. 2002.
- [2] EASTWOOD S.J., WEBB P, Mckcown C., The use of the TI2 Manufacturing System on a Double-curvature Aerospace Panel, Journal of Engineering Manufacture, Part B, Vol. 217, 2003, 849-855.
- [3] GROOVER M.P., WEISS M., NAGEL R.N, ODREV N.G., Industrial Robotics - Technology, Programming, and Applications, McGraw-Hill, New York. ISBN: 0-07-024989-X, 1986.
- [4] JAYAWEERA N, Webb P., Automated assembly of fuselage skin panels. Assembly Automation, Vol. 27, No. 4, 2007, 343-355.
- [5] JAYAWEERA N.,WEBB P., Adaptive robotic assembly of compliant aero-structure components. Robotics and Computer Integrated Manufacturing, Vol. 23, No 2, 2007, 180-194.
- [6] KAYANI A., JAMSHIDI J., Measurement assisted assembly for large volume aircraft wing structures, 4th International Conference on Digital Enterprise Technology, University of Bath, UK, 2007, 426-434. ISBN 978-0-86-197-141-1.
- [7] PARK E., MILLS K., Three Dimensional Localization of Thin Walled Sheet Metal parts for Robotic Assembly, Journal of Robotic Systems, Vol. 19 No, 5, 2002, 207-217.
- [8] PARK E., XU W., MILLS K., Calibration-based absolute localization of parts for multi-robot assembly, Robotica, Vol. 20, 2002, 359-366.
- [9] ROCHE N.R., Automatic Riveting Cell for Commercial Aircraft Floor Grid Assembly, Aerospace Engineering, Vol. 15, No. 1, 1995, 7-10.
- [10] ROOKS B., Automatic Wing Box Assembly Developments, Industrial Robot, Vol. 28, No. 4, 2001, 297-302.
- [11] WEBB P., EASTWOOD S.J., An Evaluation of the TI2 Manufacturing System for the Machining of Airframe Subassemblies, Journal of Engineering Manufacture, Part B, Vol. 218, 2004, 819-826.
- [12] WEBB P., EASTWOOD S., JAYAWEERA N., YE C., Automated Aerostructure Assembly, Industrial Robot, Vol. 32, No. 5, 2005, 383-387.
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Bibliografia
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