NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Flight evaluation of a digital electronic engine control system in an F-15 airplaneBenefits provided by a full-authority digital engine control are related to improvements in engine efficiency, performance, and operations. An additional benefit is the capability of detecting and accommodating failures in real time and providing engine-health diagnostics. The digital electronic engine control (DEEC), is a full-authority digital engine control developed for the F100-PW-100 turbofan engine. The DEEC has been flight tested on an F-15 aircraft. The flight tests had the objective to evaluate the DEEC hardware and software over the F-15 flight envelope. A description is presented of the results of the flight tests, which consisted of nonaugmented and augmented throttle transients, airstarts, and backup control operations. The aircraft, engine, DEEC system, and data acquisition and reduction system are discussed.
Document ID
19820054148
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Myers, L. P.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Mackall, K. G.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Burcham, F. W., Jr.
(NASA Ames Research Center Edwards AFB, CA, United States)
Walter, W. A.
(United Technologies Corp. Pratt and Whitney Aircraft Group, West Palm Beach, FL, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 82-1080
Meeting Information
Meeting: Joint Propulsion Conference
Location: Cleveland, OH
Start Date: June 21, 1982
End Date: June 23, 1982
Sponsors: AIAA, SAE, and ASME
Accession Number
82A37683
Distribution Limits
Public
Copyright
Other

Available Downloads

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