TY - GEN
T1 - Monotone restriction model of large-scale complex product reliability evaluation
AU - Liu, Zhiyang
AU - Liu, Lu
AU - Huang, Min
AU - Chen, Mingzhu
PY - 2009
Y1 - 2009
N2 - The development of large-scale complex product is a long time process, and the trial cost is high. Therefore, the test data of these products usually presents small sample and multiphase characteristic. To reduce the evaluation error caused by small sample of one phase, a constraint condition, which is the products' reliability increases monotonously, was introduced to products reliability evaluation, thus the multi-phase test data can be used for the reliability evaluation. Reliability of product usually increases during the development process, therefore, this method has comprehensive applicability. Under such constraint condition, the reliability parameter was considered as a random variable and the reliability parameter distribution function was given first. Then an approximate calculation method for mission reliability and MTBF was presented. Finally, take an aircraft engine for example to compare the result obtained from single phase test data with that based on multi-phase test data. Since the constraint condition is brief and the reliability parameter distribution function can be achieved, this method is more applicable for engineering than traditional AMSAA-Model, and it can gain the reliability interval estimation which can't be obtained from Duane-Model.
AB - The development of large-scale complex product is a long time process, and the trial cost is high. Therefore, the test data of these products usually presents small sample and multiphase characteristic. To reduce the evaluation error caused by small sample of one phase, a constraint condition, which is the products' reliability increases monotonously, was introduced to products reliability evaluation, thus the multi-phase test data can be used for the reliability evaluation. Reliability of product usually increases during the development process, therefore, this method has comprehensive applicability. Under such constraint condition, the reliability parameter was considered as a random variable and the reliability parameter distribution function was given first. Then an approximate calculation method for mission reliability and MTBF was presented. Finally, take an aircraft engine for example to compare the result obtained from single phase test data with that based on multi-phase test data. Since the constraint condition is brief and the reliability parameter distribution function can be achieved, this method is more applicable for engineering than traditional AMSAA-Model, and it can gain the reliability interval estimation which can't be obtained from Duane-Model.
KW - Complex system
KW - Reliability evaluation
KW - Reliability growth
KW - Small sample
UR - https://www.scopus.com/pages/publications/77955978790
U2 - 10.1109/ICRMS.2009.5270180
DO - 10.1109/ICRMS.2009.5270180
M3 - 会议稿件
AN - SCOPUS:77955978790
SN - 9781424449057
T3 - Proceedings of 2009 8th International Conference on Reliability, Maintainability and Safety, ICRMS 2009
SP - 319
EP - 322
BT - Proceedings of 2009 8th International Conference on Reliability, Maintainability and Safety, ICRMS 2009
T2 - 2009 8th International Conference on Reliability, Maintainability and Safety, ICRMS 2009
Y2 - 20 July 2009 through 24 July 2009
ER -