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Airstart performance of a digital electronic engine control system on an F100 engineThe digital electronic engine control (DEEC) system installed on an F100 engine in an F-15 aircraft was tested. The DEEC system incorporates a closed-loop air start feature in which the fuel flow is modulated to achieve the desired rate of compressor acceleration. With this logic the DEEC equipped F100 engine can achieve air starts over a larger envelope. The DEEC air start logic, the test program conducted on the F-15, and its results are described.
Document ID
19860015879
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Burcham, F. W., Jr. (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-8
Report Number: PAPER-8
Accession Number
86N25350
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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