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Introduction and Application of Modular Turbine Engine Performance Analyses System Within KLM Royal Dutch Airlines FREE

[+] Author Affiliations
Willem J. Schröder, Harmen Lanser

KLM Royal Dutch Airlines, Schiphol Airport, The Netherlands

Paper No. 89-GT-317, pp. V002T02A016; 5 pages
doi:10.1115/89-GT-317
From:
  • ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
  • Toronto, Ontario, Canada, June 4–8, 1989
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7914-6
  • Copyright © 1989 by ASME

abstract

KLM Royal Dutch Airlines has successfully been using the General Electric Ground-based Engine Monitoring (GEM) system for overall monitoring of on-wing engines for several years.

GEM provides a function for the modular analysis of engines with the Turbine Engine Modular Performance Estimation Routine (TEMPER).

This paper describes the introduction and first applications of the Test Cell TEMPER routine within KLM for the CF6-50 and CF6-80 engines.

The subjects to be discussed include a short description, the installation and the evaluation of the Test Cell TEMPER function. Furthermore, KLM’s first experience with Test Cell TEMPER and KLM’s plans with TEMPER for the near future are discussed.

Copyright © 1989 by ASME
Topics: Gas turbines
This article is only available in the PDF format.

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