NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Fuel consumption improvement in current transport enginesA review is conducted of improvements which can be made with respect to the fuel consumption of current engines and new production versions of current engines. A description is presented of an engine diagnostics program which has the objective to identify and quantify the causes and sources of performance deterioration in the JT9D turbofan engine and to develop basic data which will be applied to minimize performance degradation of current and future engines. General areas where performance losses occur are examined, taking into account seals, blades and vanes, and cases. Potential performance improvement concepts are related to improved component aerodynamics, improved flowpath sealing, blade tip clearance control, improved turbine cooling effectiveness, improved turbine materials and coatings, duct and nozzle aerodynamic refinements, nacelle aerodynamic refinements, forced exhaust mixers, advanced nacelle materials, and advanced fuel control.
Document ID
19780061188
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hines, R. W.
(United Technologies Corp. Pratt and Whitney Aircraft Group, East Hartford, Conn., United States)
Ziemianski, J. A.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
July 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 78-930
Meeting Information
Meeting: Joint Propulsion Conference
Location: Las Vegas, NV
Country: US
Start Date: July 25, 1978
End Date: July 27, 1978
Sponsors: American Institute of Aeronautics and Astronautics, Society of Automotive Engineers
Accession Number
78A45097
Funding Number(s)
CONTRACT_GRANT: NAS3-20632
CONTRACT_GRANT: NAS3-20630
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available