The U.S. Air Force and Pratt & Whitney Aircraft are currently engaged in developing technology to minimize low-cycle fatigue maintenance requirements in future gas turbine engines. The Life Cycle Cost/Damage Tolerance Assessment (LCC/DTA) program is directed toward furthering technology development in two important areas that relate to the overall life cycle cost of advanced Air Force weapon systems: life cycle cost modeling and analysis, and damage tolerance design (DTD). A major goal of the LCC/DTA program is to establish hot-section disk design criteria specifying acceptable levels for life and maintenance actions based on minimum life cycle cost. This paper discusses the methodology developed to evaluate the weapon system LCC impact of designing to damage tolerance criteria.
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ASME 1983 International Gas Turbine Conference and Exhibit
March 27–31, 1983
Phoenix, Arizona, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7952-8
PROCEEDINGS PAPER
EAGLE/DTA: A Life Cycle Cost Model for Damage Tolerance Assessment
Edward J. Reed
Edward J. Reed
Pratt & Whitney Aircraft, West Palm Beach, FL
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Edward J. Reed
Pratt & Whitney Aircraft, West Palm Beach, FL
Paper No:
83-GT-76, V002T02A004; 6 pages
Published Online:
April 7, 2015
Citation
Reed, EJ. "EAGLE/DTA: A Life Cycle Cost Model for Damage Tolerance Assessment." Proceedings of the ASME 1983 International Gas Turbine Conference and Exhibit. Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. Phoenix, Arizona, USA. March 27–31, 1983. V002T02A004. ASME. https://doi.org/10.1115/83-GT-76
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