Energy Efficient Engine Program: Technology Benefit/Cost Study, Volume IIThe Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development and Integration program was successful in achieving its objectives: identification of air transport propulsion system technology requirements for the years 2000 and 2010, and formulation of programs for developing these technologies. It is projected that the advanced technologies identified, when developed to a state of readiness, will provide future commercial and military turbofan engines with significant savings in fuel consumption and related operating costs. These benefits are significant and far from exhausted. The potential savings translate into billions of dollars in annual savings for the airlines. Analyses indicate that a significant portion of the overall savings is attributed to aerodynamic and structure advancements. Another important consideration in acquiring these benefits is developing a viable reference technology base that will permit engines to operate at substantially higher overall pressure ratios and bypass ratios. Results have pointed the direction for future research and a comprehensive program plan for achieving this was formulated. The next major step is initiating the program effort that will convert the advanced technologies into the expected benefits.
Document ID
19900019249
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Gray, D. E. (Pratt and Whitney Aircraft East Hartford, CT, United States)
Gardner, W. B. (Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PWA-5594-251-VOL-2NASA-CR-174766-VOL-2NAS 1.26:174766-VOL-2Report Number: PWA-5594-251-VOL-2Report Number: NASA-CR-174766-VOL-2Report Number: NAS 1.26:174766-VOL-2