Relative change of thermodynamic parameters of a flowing part two spool mixed flow turbofan after repair at an exhaustion of resource

Authors

  • Bulat Rinatovich Abdullin
  • Vladimir Petrovich Alatorcev
  • Aleksandr Vitalevich Gumerov
  • Haydar Sagitovich Gumerov

Keywords:

Авиационный газотурбинный двигатель ; ремонт ; проточная часть ; зазор ; эксплуатационный дефект

Abstract

In this method thermodynamic parameters of the repaired and new engines for an estimation of quality of the repaired engines are compared. 

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Published

2018-13-09

Issue

Vol. 12 No. 2 (31) (2009): Вестник УГАТУ

Section

MECHANICAL ENGINEERING AND ENGINEERING SCIENCE