TECHNICAL PAPERS

Calculation of Control Laws for the Digital Fuel Control Unit of a Small Thrust Turbojet

Date Published: 1993-04-01
Paper Number: 931411
DOI: 10.4271/931411

Citation:

Torella, G. and Liotti, G., "Calculation of Control Laws for the Digital Fuel Control Unit of a Small Thrust Turbojet," SAE Technical Paper 931411, 1993, doi:10.4271/931411.

Author(s):


G. Torella - Italian Air Force Academy
G. Liotti - Alfa Romeo Avio S. p. A

Abstract:

The methods and the techniques set-up for evaluating the control laws for the digital main fuel control unit (MFCU) of a small thrust turbojet engine are shown. A suitable parameter defining the surge margin is considered. The paper deals with the results of a study carried out in order to evaluate the influence of engine operating parameters on the surge margin. For this aim the steady state engine simulation programs, based on the state vector technique, have proved to be very effective. Finally the codes and the obtained results have been used for calculating some suitable control laws for a digital MFCU.

File Size: 1410K

Product Status: In Stock

See papers presented at Aerospace Atlantic Conference & Exposition, April 1993, Dayton, OH, USA, Session: Aerospace Atlantic Conference & Exposition

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