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Computer Systems: An Aid to the Development of Gas Turbine Engines PUBLIC ACCESS

[+] Author Affiliations
H. Schneider

KHD Luftfahrttechnik GmbH, Oberursel/Ts., West Germany

Paper No. 83-GT-110, pp. V002T02A008; 8 pages
doi:10.1115/83-GT-110
From:
  • ASME 1983 International Gas Turbine Conference and Exhibit
  • Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
  • Phoenix, Arizona, USA, March 27–31, 1983
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7952-8
  • Copyright © 1983 by ASME

abstract

This paper presents a concept as to the stepwise extension of computer-systems application by KHD Luftfahrttechnik’s engineering departments engaged in gas turbine engine development.

A base line system is in used today and criteria have been established to expand this into an efficient engineering tool.

Discussed are the principle conditions and targets including items such as cost effectiveness, data communications between different departments, programming, personnel training as well as data analysis and requirements for soft and hardware.

Copyright © 1983 by ASME
This article is only available in the PDF format.

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