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Improved components for engine fuel savingsNASA programs for developing fuel saving technology include the Engine Component Improvement Project for short term improvements in existing air engines. The Performance Improvement section is to define component technologies for improving fuel efficiency for CF6, JT9D and JT8D turbofan engines. Sixteen concepts were developed and nine were tested while four are already in use by airlines. If all sixteen concepts are successfully introduced the gain will be fuel savings of more than 6 billion gallons over the lifetime of the engines. The improvements include modifications in fans, mounts, exhaust nozzles, turbine clearance and turbine blades.
Document ID
19810049748
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Antl, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Mcaulay, J. E.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
SAE PAPER 801116
Meeting Information
Meeting: Aerospace Congress and Exposition
Location: Los Angeles, CA
Start Date: October 13, 1980
End Date: October 16, 1980
Sponsors: Society of Automotive Engineers
Accession Number
81A34152
Distribution Limits
Public
Copyright
Other

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