DocumentCode
2471126
Title
The study of the helicopter rotor prognostic method and health management system based-on FMA
Author
Fang, Hongzheng ; Xiong, Yi ; Luo, Kai ; Han, Liming
Author_Institution
Beijing Aerosp. Meas. & Control Corp., Beijing, China
fYear
2012
fDate
23-25 May 2012
Firstpage
1
Lastpage
8
Abstract
Helicopter rotor system consists of a large number of dynamic components, and works in a single-channel and complex environment, which is a critical system that ensures the helicopter reliability and security. Because the data on the rotating parts is not easy to measure, and the noise environment is complex, the rotor fault detection capacity is limited, thus seriously affecting the reliability and safety of the helicopter as a whole. This paper firstly presents the simulation of neural network prognostic method based on the rotor system failure mechanism and failure mode analysis (FMA), which can effectively use the failure mode for the modeling of the prediction method combined with the test and simulation data of key components, and greatly improved the effectiveness of fault detection. Besides, a general, open architecture of an advanced health usage and management system (A-HUMS) is proposed, and the overall structure, hierarchy and functions are elaborated. Finally, taking the helicopter rotor system components as the research object, the validation system of the helicopter HUMS system has been planned and designed. The analysis results show that the proposed method can effectively predict to preset a variety of fault conditions and solve the low predictive ability of key components of the rotor system failure problems.
Keywords
aerospace components; aerospace safety; failure analysis; helicopters; maintenance engineering; rotors; security; A-HUMS; FMA; advanced health usage and management system; complex environment; dynamic components; failure mode analysis; fault conditions; fault detection; health management system; helicopter HUMS system; helicopter reliability; helicopter rotor prognostic method; helicopter rotor system; helicopter safety; helicopter security; network prognostic method; predictive ability; rotating parts; rotor fault detection capacity; rotor system failure problems; single-channel environment; Absorption; Analytical models; Blades; Computer architecture; Friction; Moisture; FMA; HUMS; architecture; helicopter; prognostic; rotor system;
fLanguage
English
Publisher
ieee
Conference_Titel
Prognostics and System Health Management (PHM), 2012 IEEE Conference on
Conference_Location
Beijing
ISSN
2166-563X
Print_ISBN
978-1-4577-1909-7
Electronic_ISBN
2166-563X
Type
conf
DOI
10.1109/PHM.2012.6228933
Filename
6228933
Link To Document