4.6 Article

Two new multi-phase reliability growth models from the perspective of time between failures and their applications

Journal

CHINESE JOURNAL OF AERONAUTICS
Volume 34, Issue 5, Pages 341-349

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.cja.2020.12.017

Keywords

Reliability growth; Test-find-test strategy; Test-fix-test strategy; Time-varying failure inten-sity; Time between failures

Funding

  1. National Natural Science Foundation of China [52075019]
  2. Academic Excellence Foundation of BUAA for PhD Students, China

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Two new reliability growth models have been proposed to address the problem of constant failure intensity assumption in each phase, which outperform existing models according to applications with real data.
Aviation products would go through a multi-phase improvement in reliability perfor-mance during the research and development process. In the literature, most of the existing reliability growth models assume a constant failure intensity in each test phase, which inevitably limits the scope of the application. To address this problem, we propose two new models considering time-varying failure intensity in each stage. The proposed models borrow the idea from the accelerated failure-time models. It is assumed that time between failures follow the log-location-scale distribu-tion and the scale parameters in each phase do not change, which forms the basis for integrating the data from all test stages. For the test-find-test scenario, an improvement factor is introduced to con-struct the relationship between two successive location parameters. Whereas for the test-fix-test sce-nario, the instantaneous cumulative time between failures is assumed to be consistent with Duane model and derive the formulation of location parameter. Likelihood ratio test is further utilized to test whether the assumption of constant failure intensity in each phase is suitable. Several applica-tions with real reliability growth data show that the assumptions are reasonable and the proposed models outperform the existing models. (c) 2020 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).

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