Al-Habaideh2.pdf (1.22 MB)
Experimental design and investigation of a pin-type reconfigurable clamping system for manufacturing aerospace components
journal contributionposted on 2009-05-26, 09:50 authored by A. Al-Habaibeh, N. Gindy, Robert M. Parkin
This paper presents an experimental design and evaluation of a pin-type universal clamping system. The clamping system is designed for holding complex-shaped aerospace components, such as turbine blades, during machining processes. The experimental investigation is performed by comparing the pin-type clamping system with a dedicated clamping system during the machining of aluminium and steel parts. Force signals are monitored during machining. The experimental results are presented and compared with a dedicated clamping system. From the comparison, the performance of the clamping system is discussed. The results provide an evaluation of the designed pin-type clamping systems for machining operations. The results prove that the pin-type clamping system can be reconfigured for machining different complex shaped components with performance comparable with a dedicated clamping system.
- Mechanical, Electrical and Manufacturing Engineering
CitationAL-HABAIBEH, A., GINDY, N. and PARKIN, R.M., 2003. Experimental design and investigation of a pin-type reconfigurable clamping system for manufacturing aerospace components. Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture, 217(12), pp. 1771-1777.
PublisherProfessional Engineering Publishing / © IMECHE
- VoR (Version of Record)
NotesThis is an article from the journal, Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture [© IMechE ]. It is also available at: http://dx.doi.org/10.1243/095440503772680703