Thrust control malfunction accommodation system and method

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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F01D 21/00 (2006.01) B64D 31/00 (2006.01) F01D 21/14 (2006.01) F02C 9/00 (2006.01) F02C 9/46 (2006.01)

Patent

CA 2424251

A system for detecting and correcting a thrust control malfunction in an aircraft engine. The system includes an electronic engine control (EEC) unit that includes a first processing subsystem and a second processing subsystem, and a thrust control malfunction accommodation (TCMA) circuit included in the first processing subsystem and the second processing subsystem. Additionally, the system includes a TCMA software package executed by the first processing subsystem and the second processing subsystem, thereby providing redundant execution of the TCMA software package.

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