Title :
Notice of Retraction
Physical failure analysis of A320 flap based on DMU
Author :
Wei Tian ; Weimin Cui ; Shijian Zhao
Author_Institution :
Sch. of Aeronaut., Northwestern Polytech. Univ., Xi´an, China
Abstract :
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
Flap mechanism is sophisticated and one part failure often affect other parts. This article mainly analyzes the physical failures of key parts in A320 flap and interactions of different components´ physical failures. To analyze the interactions of different components, DMU is used to compute the collision, clearance and contact between them. At the same time, by introducing the concept of weighting factor, the interactions of different components is reflected in the form of formulas, which makes it possible to calculate the quantitative reliability affected by other mechanisms.
Keywords :
aerospace components; aircraft; failure analysis; reliability; DMU; airbus A320 flap mechanism; component physical failure analysis; contact; digital mock-up; part failure; reliability; Actuators; Analytical models; Electron tubes; Failure analysis; Joints; Reliability; Torque; A320 flap; DMU; interaction; physical failure; weighting factor;
Conference_Titel :
Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE), 2013 International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4799-1014-4
DOI :
10.1109/QR2MSE.2013.6625716
