THE APPLICATION OF A DESIGN VERIFICATION SYSTEM AND ACCELERATED MISSION TESTING TO GAS TURBINE ENGINE DEVELOPMENT

780991

2/1/1978

Authors
Abstract
Content
Two advanced techniques to improve the process of designing and developing high technology gas turbine engines are being evaluated and implemented at the Pratt & Whitney Aircraft Government Products Division:
  • Improved Design Verification System
  • Accelerated Mission Endurance Test Techniques.
These techniques are not new, but they have been significantly improved and strengthened in the past few years by the development of new high technology instrumentation and sophisticated computerized design prediction methods. These tools are aimed at providing improved product reliability during the early operational phase and reducing ultimate cost of ownership for the user.
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DOI
https://doi.org/10.4271/780991
Citation
McDonnell, B., "THE APPLICATION OF A DESIGN VERIFICATION SYSTEM AND ACCELERATED MISSION TESTING TO GAS TURBINE ENGINE DEVELOPMENT," Aerospace Meeting, San Diego, California, United States, November 27, 1978, https://doi.org/10.4271/780991.
Additional Details
Publisher
Published
2/1/1978
Product Code
780991
Content Type
Technical Paper
Language
English