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The GTCP36-300, a Gas Turbine Auxiliary Power Unit for Advanced Technology Transport Aircraft FREE

[+] Author Affiliations
L. M. Stohlgren

Garrett Turbine Engine Company, Phoenix, AZ

Lutz D. Werner

Garrett GmbH, West Germany

Paper No. 86-GT-285, pp. V002T04A011; 9 pages
doi:10.1115/86-GT-285
From:
  • ASME 1986 International Gas Turbine Conference and Exhibit
  • Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
  • Dusseldorf, West Germany, June 8–12, 1986
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7929-0
  • Copyright © 1986 by ASME

abstract

The Garrett GTCP36-300 Series Auxiliary Power Unit is being developed for use on advanced technology transport aircraft in the 150-passenger size class. The first application will be the Airbus Industries A320 Aircraft. The APU uses a 6:1 pressure ratio, single-stage compressor and turbine, driving a single-stage load compressor and accessory gearbox. The 480 horsepower APU delivers compressed air to the aircraft pneumatic system and drives a customer furnished 90 kva, 24,000 rpm electrical generator. State-of-the-art aerodynamics, materials, and digital electronics are used to give the user-airlines an APU delivering maximum performance with minimum envelope, weight, and cost of ownership.

Copyright © 1986 by ASME
This article is only available in the PDF format.

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