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Collaborative Engineering in Integrated Aircraft Power System Design

[+] Author Affiliations
Robert L. Bayt, Michael K. Sahm

United Technologies Research Center, East Hartford, CT

Charles E. Lents

Hamilton Sundstrand, Rockford, IL

Paper No. DETC2002/ISD-34439, pp. 371-375; 5 pages
doi:10.1115/DETC2002/ISD-34439
From:
  • ASME 2002 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
  • Volume 4: 14th International Conference on Design Theory and Methodology, Integrated Systems Design, and Engineering Design and Culture
  • Montreal, Quebec, Canada, September 29–October 2, 2002
  • Conference Sponsors: Design Engineering Division, Computers and Information in Engineering Division
  • ISBN: 0-7918-3624-X
  • Copyright © 2002 by ASME

abstract

Integrated aircraft power system design can provide for performance increases, weight reductions, and cost reductions by exploiting synergies and opportunities for functional integration between systems. A method for bringing together discipline expertise into a common environment for defining system specifications and interfaces that exploit these synergies is presented here. The goal is to create the broadest possible use of the trade-space for aircraft applications. An integrated process and tool environment are described. This process has been applied in the areas of airframe-propulsion integration, thermal management and environmental control systems, control system integration and in the evaluation of more electric aircraft architectures.

Copyright © 2002 by ASME

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