A disturbed combustion process in an aircraft engine has an
impact on the internal flow and leads to specific irregularities in the
species distribution in the exhaust jet. Measuring this distribution
provides information about the combustion state and offers the
possibility to reduce the engine down-time during inspection. The
approach has the potential to improve the resource management as
well as the availability and safety of the system. Aim of the research
project is to evaluate the state of an aircraft engine by analyzing the
emission field in the exhaust jet and using a support vector machine
(SVM) algorithm for automatic defect detection and allocation.
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