posted on 2018-05-18, 08:56authored byPaul J. Highmore
In the field of non-destructive testing there exists the
particular problem of examining adhesively-bonded, multi-layered
structures for bonding defects and delaminations.
An example of such a structure is part of a proposed Rolls-Royce
fan blade intended for use in the first stage of a turbo-fan aero engine.
The bulk of the blade is made up of a carbon-fibre composite material
but the leading edge is reinforced by several adhesively-bonded, stainless
steel layers. It is necessary in this case to be able to find—non-destructively—the existence of any non-bonded areas and, of equal
importance, their depth locations. [Continues.]
Funding
Great Britain, Ministry of Defence, Procurement Executive.
History
School
Mechanical, Electrical and Manufacturing Engineering
This work is made available according to the conditions of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/
Publication date
1973
Notes
A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy at Loughborough University.