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Analysis of the impact of the use of broad specification fuels on combustors for commercial aircraft gas turbine enginesAn analytical study was conducted to assess the impact of the use of broad specification fuels with reduced hydrogen content on the design, performance, durability, emissions and operational characteristics of combustors for commercial aircraft gas turbine engines. The study was directed at defining necessary design revisions to combustors designed for use of Jet A when such are operated on ERBS (Experimental Referee Broad Specification Fuel) which has a nominal hydrogen content of 12.8 percent as opposed to 13.7 percent in current Jet A. The results indicate that improvements in combustor liner cooling, and/or materials, and methods of fuel atomization will be required if the hydrogen content of aircraft gas turbine fuel is decreased.
Document ID
19790054967
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Szetela, E. J.
(United Technologies Research Center East Hartford, Conn., United States)
Lehmann, R. P.
(United Technologies Corp. Pratt and Whitney Aircraft Group, East Hartford, Conn., United States)
Smith, A. L.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Subject Category
Propellants And Fuels
Report/Patent Number
AIAA PAPER 79-1195
Meeting Information
Meeting: AIAA, SAE, and ASME, Joint Propulsion Conference
Location: Las Vegas, NV
Start Date: June 18, 1979
End Date: June 20, 1979
Sponsors: ASME, AIAA, SAE
Accession Number
79A38980
Distribution Limits
Public
Copyright
Other

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