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Advanced controls for airbreathing engines, volume 3: Allison gas turbineThe application of advanced control concepts to airbreathing engines may yield significant improvements in aircraft/engine performance and operability. Screening studies of advanced control concepts for airbreathing engines were conducted by three major domestic aircraft engine manufacturers to determine the potential impact of concepts on turbine engine performance and operability. The purpose of the studies was to identify concepts which offered high potential yet may incur high research and development risk. A target suite of proposed advanced control concepts was formulated and evaluated in a two-phase study to quantify each concept's impact on desired engine characteristics. To aid in the evaluation specific aircraft/engine combinations were considered: a Military High Performance Fighter mission, a High Speed Civil Transport mission, and a Civil Tiltrotor mission. Each of the advanced control concepts considered in the study are defined and described. The concept potential impact on engine performance was determined. Relevant figures of merit on which to evaluate the concepts are determined. Finally, the concepts are ranked with respect to the target aircraft/engine missions. A final report describing the screening studies was prepared by each engine manufacturer. Volume 3 of these reports describes the studies performed by the Allison Gas Turbine Division.
Document ID
19940007800
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bough, R. M.
(General Motors Corp. Indianapolis, IN, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-8007
NASA-CR-189205
NAS 1.26:189205
Report Number: E-8007
Report Number: NASA-CR-189205
Report Number: NAS 1.26:189205
Accession Number
94N12272
Funding Number(s)
PROJECT: RTOP 505-62-41
CONTRACT_GRANT: NAS3-25459
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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