Estimation of probability of efficiency of parametrical diagnosing of the condition aviation gas-turbing

Abstract

The method of an estimation of efficiency of parametrical diagnosing of a condition aviation gasturbine, is considered by estimated probability of recognition of a defective condition. The estimation is carried out in two stages. At the first stage functions of distribution and confidential borders of criteria of defects (parameters of a condition) aviation gas-turbine are defined. At the second stage estimate efficiency of existing methods of identification of a condition. For final the method, with the greatest probability of recognition is accepted.