Method and apparatus for curing a composite article
AssigneeSpirit Aerosystems (Europe) Limited
InventorsAndrew W. Hamilton, Christos Tachtatzis
Life of this patent
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AssigneeSpirit Aerosystems (Europe) Limited
InventorsAndrew W. Hamilton, Christos Tachtatzis
Estimating the term…
Disclosed is a method of curing a composite article and associated curing apparatus. A heat source is provided for heating the composite article. A temperature related property is detected proximal to the heat source and the heat output is regulated to a predetermined temperature vs. time profile. Heat output vs time data is acquired and functionalised and the curing completion time is determined based on the functionalised heat output vs time data. The method provides for heating a composite article so as to follow a predetermined temperature vs. time profile (i.e. a cure profile) and avoid excessively high temperatures. The required heat output vs time has also been found to be broadly reproducible, and the curing completion time can be more readily determined from functionalised heat output vs time data, for example by identifying reproducible characteristics of the functionalised data.
A method of curing a composite article, comprising;
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