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Augmentor transient capability of an F100 engine equipped with a digital electronic engine controlAn F100 augmented turbofan engine equipped with digital electronic engine control (DEEC) system was evaluated. The engine was equipped with a specially modified augmentor to provide improved steady state and transient augmentor capability. The combination of the DEEC and the modified augmentor was evaluated in sea level and altitude facility tests and then in four different flight phases in an F-15 aircraft. The augmentor configuration, logic, and test results are presented.
Document ID
19860015882
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Burcham, F. W., Jr. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Pai, G. D. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 12, 2013
Publication Date
March 1, 1984
Publication Information
Publication: Digital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 Airplane
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PAPER-11
Report Number: PAPER-11
Accession Number
86N25353
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19860015871Collected WorksDigital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 Airplane19860015871Collected WorksDigital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 Airplane
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