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Digital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 AirplaneFlight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. Topics discussed include: system description, F100 engine tests, effects of inlet distortion on static pressure probe, flight tests, digital electronic engine control fault detection and accommodation flight evaluation, flight evaluation of a hydromechanical backup control, augmentor transient capability of an F100 engine, investigation of nozzle instability, real time in flight thrust calculation, and control technology for future aircraft propulsion systems. It is shown that the DEEC system is a powerful and flexible controller for the F100 engine.
Document ID
19860015871
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
September 5, 2013
Publication Date
March 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
H-1201
NAS 1.55:2298
NASA-CP-2298
Accession Number
86N25342
Funding Number(s)
PROJECT: RTOP 533-02-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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