Propulsion Control Integration for Power Management

700818

2/1/1970

Authors
Abstract
Content
Integration of propulsion controls can simplify the task of aircraft power management. Not only can integration ease the pilot's problem of adjusting engine power settings according to the flight mode, but it also enables improved propulsion system performance to be achieved and extends the regions of safe and stable operation. Such improvements to the inlet/engine compatibility by themselves warrant the use of control system integration, but once the controls are adapted for ease of data exchange they can easily accommodate power management functions and the processing of parameters for a maintenance monitor. One possible method of implementation is described utilizing state-of-the-art hardware.
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DOI
https://doi.org/10.4271/700818
Citation
Flanders, T. and Britnell, W., "Propulsion Control Integration for Power Management," National Aeronautic and Space Engineering and Manufacturing Meeting, Los Angeles, California, United States, October 5, 1970, https://doi.org/10.4271/700818.
Additional Details
Publisher
Published
2/1/1970
Product Code
700818
Content Type
Technical Paper
Language
English