Information technology for adjustment of dynamic processes in aircraft gas turbine engines during the acceptance tests

The aids of simulation that are used to automate the adjustment of aircraft GTE control systems are described. A technique of the information technology for adjustment of a control system by turning on the afterburner and results of its practical application during the acceptance tests in series pro...

Full description

Saved in:
Bibliographic Details
Published in:Russian aeronautics 2007-09, Vol.50 (3), p.268-276
Main Authors: Akhmedzyanov, D. A., Kishalov, A. E.
Format: Article
Language:English
Subjects:
Acceptance tests
Aerospace engines
Afterburners
Aids
Aircraft
Control systems
Gas turbine engines
Information systems
Mathematical models
Studies
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:The aids of simulation that are used to automate the adjustment of aircraft GTE control systems are described. A technique of the information technology for adjustment of a control system by turning on the afterburner and results of its practical application during the acceptance tests in series production are presented. Also given is a model for the process of afterburner ignition and reaching the power augmented conditions of the engine.[PUBLICATION ABSTRACT]
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799807030063