DocumentCode :
2664488
Title :
System engineering approach for diagnostics of electromechanical systems
Author :
Dumont, Paul T.
Author_Institution :
Viterbi Sch. of Eng., USC, Los Angeles, CA, USA
fYear :
2015
fDate :
26-29 Jan. 2015
Firstpage :
1
Lastpage :
7
Abstract :
Complex electromechanical subsystems have a number of electrical and mechanical components that make it difficult to fault-isolate a failure. Some electromechanical subsystems are: engine controls (Full Authority Digital Engine Control-FADEC), Environmental Control System (ECS), Auxiliary Power Unit (APU), Air-Turbine Starter Set (ATSS), Electrical Power System (EPS), mechanical Flight Control System (includes hydraulics and servo-actuators), anti-skid brake system, traction control, Fuel subsystem and anti-collision system. These have a number of electrical and mechanical components that are difficult to fault-isolate This paper provides an overall system-level approach for the implementation of a Health Management Fault Isolator (HMFI). The HMFI can be applied to a number of different systems (products) which contain electromechanical systems (subsystems) that are difficult to fault-isolate. This paper focuses on systems related to aircraft however, other systems on ships, submarines, locomotives, trucks, power plants, office buildings, wind turbines, refineries, farm equipment, tanks and automobiles can also benefit from the Health Management Fault Isolator. There are some challenges in the implementation of the HMFI that have been discussed in this paper. The initial proposal for the HMFI project must include the complete life cycle cost for the system with HMFI and the complete life cycle cost for the same system without HMFI.
Keywords :
aerospace engines; aircraft; condition monitoring; fault diagnosis; life cycle costing; systems engineering; ECS; FADEC; HMFI; air turbine starter set; aircraft; auxiliary power unit; electrical power system; electromechanical subsystem diagnostics; environmental control system; failure analysis; fault isolation; full authority digital engine control; health management fault isolator; life cycle costing; mechanical flight control system; system engineering; Aerospace electronics; Aircraft; Circuit faults; Engines; Monitoring; Temperature sensors; Valves; fault isolator; health management; system level analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability and Maintainability Symposium (RAMS), 2015 Annual
Conference_Location :
Palm Harbor, FL
Print_ISBN :
978-1-4799-6702-5
Type :
conf
DOI :
10.1109/RAMS.2015.7105122
Filename :
7105122
Link To Document :
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