Technical state estimation of running aircraft gas turbine engine, which is based ontransitionaland semi-permanent process

Authors

  • Haydar Sagitovich Gumerov
  • Ildar Vakilevich Salimov

Keywords:

Контроль технического состояния; авиационный газотурбинный двигатель; переходные и транспереходные процессы

Abstract

Investigations are realized and algorithms of control of working process parameters at non-stationary modes are developed for monitoring of technical state of aviation gas turbine engines in maintenance.

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Published

2018-07-08

Issue

Vol. 10 No. 1 (26) (2008): Вестник УГАТУ

Section

MECHANICAL ENGINEERING AND ENGINEERING SCIENCE