Method of Spare Parts: Digital Simulation of Aircraft Turbine Engine Control System

Author(s):  
Guan Yan-Shen ◽  
Warng Juhng-Sheng ◽  
Lee Tzu-Cheng

The paper presents a new method of digital simulation of a control system. A computer program of an aircraft engine control system, as for an example, is implemented as a full authority digital simulator. The results of simulation show that the functions and applications of the simulator are extended as compared with those of the other type mathematical simulators.

2011 ◽  
Vol 14 (4) ◽  
pp. 52-56
Author(s):  
Seong-Jin Hong ◽  
Seung-Min Kim ◽  
Sim-Kyun Yook ◽  
Sam-Sik Nam

Author(s):  
Li-Chieh Hsu ◽  
Wu-Chi Ho ◽  
Chien-Ching Hsueh

A novel Air Start Unit powered by gas turbine engine is developed. The feature of this unit is that it can start various aircraft engines, including the hundred thousand pound thrust class engine like GE90, with different air flow rate in a compact design. This paper introduces the complete design and development of large centrifugal compressor, digital engine control system, testing of gas turbine system.


2004 ◽  
Vol 37 (6) ◽  
pp. 1049-1053
Author(s):  
A.S. Kulik ◽  
V.F. Symonov ◽  
S.N. Pasichnik ◽  
A.V. Komkov

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