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Development of a Compact Real-Time Turbofan Engine Dynamic Simulation Aircraft Engine Business Group General Electric Company

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
French, Michael W., author.
Conference Name:
Aerospace Congress & Exposition (1982-10-25 : Anaheim, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1982
Summary:
Recent developments in the area of digital propulsion controls have precipitated requirements for compact real-time dynamic engine simulations. This paper describes the analytical development and experimental validation of a full range, non-linear model of the F404-GE-400 afterburning turbofan engine. Unique approaches were used to obtain a highly compact model which is capable of being operated in an engine mounted airborne digital computer. The model served as a signal source in a failure protection scheme, providing an unusual basis for model validation. Highlights of the very successful broad ranging validation and use of this model* are provided
Notes:
Vendor supplied data
Publisher Number:
821401
Access Restriction:
Restricted for use by site license

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