Experimental design and investigation of a pin-type reconfigurable clamping system for manufacturing aerospace components-Reference-Cited by-同舟云学术

Experimental design and investigation of a pin-type reconfigurable clamping system for manufacturing aerospace components

Published:2003-12-01 Issue:12 Volume:217 Page:1771-1777
ISSN:0954-4054
Container-title:Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture

Author:

Al-Habaibeh A¹,Gindy N²,Parkin R M¹

Affiliation:

1. Loughborough University Mechatronics Research Centre, Wolfson School of Mechanical and Manufacturing Engineering Leicestershire, UK

2. University of Nottingham School of Mechanical, Materials, Manufacturing Engineering and Management UK

Abstract

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.

Publisher

SAGE Publications

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1243/095440503772680703

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