Expert system for an estimation of conformity of the plane configuration to AP-25 requirements regarding engine rotor burst
Mechanical Engineering
Аuthors
*, **Company «Tupolev», 17, nab. Akademika Tupoleva, Moscow, 105005, Russia
*e-mail: mitin_ia@mail.ru
**e-mail: nikulochkinm@rambler.ru
Abstract
The methods and results of working out of expert system for the analysis of configurations of planes about conformity to standard documents of the Aviaregister of Interstate Aviation Committee (AR IAC) are presented. Methods of reception and the analysis of initial data in the environment of CAD/CAM system ProEngineer are stated, examples of work of subprograms of system are shown at checks of configurations of planes. Preliminary results are received.Keywords:
non-localized dispersion of the mass of the engine; configuration systems; risk ratio; degree of risk; the angle of defeat; the chances of failure; the chances of a catastrophic situation; the chances of a catastrophic situation the aircraft; the mechanism of measuring angles; the model of failure of functional systems.Download