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Author:

Bai, Bin (Bai, Bin.) | Zhang, Wei (Zhang, Wei.) | Li, Botong (Li, Botong.) | Li, Chao (Li, Chao.) | Bai, Guangchen (Bai, Guangchen.)

Indexed by:

EI Scopus SCIE

Abstract:

For the nondeterministic factors of an aeroengine blisk, including both factors with sufficient and insufficient statistical data, based on the dynamic substructural method of determinate analysis, the extremum response surface method of probabilistic analysis, and the interval method of nonprobabilistic analysis, a methodology called the probabilistic and nonprobabilistic hybrid reliability analysis based on dynamic substructural extremum response surface decoupling method (P-NP-HRA-DS-ERSDM) is proposed. The model includes random variables and interval variables to determine the interval failure probability and the interval reliability index. The extremum response surface function and its flow chart of mixed reliability analysis are given. The interval analysis is embedded in the most likely failure point in the iterative process. The probabilistic analysis and nonprobabilistic analysis are investigated alternately. Tuned and mistuned blisks are studied in a complicated environment, and the results are compared with the Monte Carlo method (MCM) and the multilevel nested algorithm (MLNA) to verify that the hybrid model can better handle reliability problems concurrently containing random variables and interval variables; meanwhile, it manifests that the computational efficiency of this method is superior and more reasonable for analysing and designing a mistuned blisk. Therefore, this methodology has very important practical significance.

Keyword:

Author Community:

  • [ 1 ] [Bai, Bin]Beijing Univ Technol, Coll Mech Engn Appl Elect Technol, Pingleyuan 100, Beijing 100022, Peoples R China
  • [ 2 ] [Zhang, Wei]Beijing Univ Technol, Coll Mech Engn Appl Elect Technol, Pingleyuan 100, Beijing 100022, Peoples R China
  • [ 3 ] [Li, Botong]Beijing Univ Technol, Coll Mech Engn Appl Elect Technol, Pingleyuan 100, Beijing 100022, Peoples R China
  • [ 4 ] [Bai, Bin]Beijing Univ Technol, Beijing Key Lab Nonlinear Vibrat & Strength Mech, Pingleyuan 100, Beijing 100022, Peoples R China
  • [ 5 ] [Zhang, Wei]Beijing Univ Technol, Beijing Key Lab Nonlinear Vibrat & Strength Mech, Pingleyuan 100, Beijing 100022, Peoples R China
  • [ 6 ] [Li, Botong]Beijing Univ Technol, Beijing Key Lab Nonlinear Vibrat & Strength Mech, Pingleyuan 100, Beijing 100022, Peoples R China
  • [ 7 ] [Bai, Bin]Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
  • [ 8 ] [Zhang, Wei]Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
  • [ 9 ] [Li, Chao]Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
  • [ 10 ] [Bai, Guangchen]Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China

Reprint Author's Address:

  • [Bai, Bin]Beijing Univ Technol, Coll Mech Engn Appl Elect Technol, Pingleyuan 100, Beijing 100022, Peoples R China;;[Zhang, Wei]Beijing Univ Technol, Coll Mech Engn Appl Elect Technol, Pingleyuan 100, Beijing 100022, Peoples R China;;[Bai, Bin]Beijing Univ Technol, Beijing Key Lab Nonlinear Vibrat & Strength Mech, Pingleyuan 100, Beijing 100022, Peoples R China;;[Zhang, Wei]Beijing Univ Technol, Beijing Key Lab Nonlinear Vibrat & Strength Mech, Pingleyuan 100, Beijing 100022, Peoples R China

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Source :

INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING

ISSN: 1687-5966

Year: 2017

Volume: 2017

1 . 4 0 0

JCR@2022

ESI Discipline: ENGINEERING;

ESI HC Threshold:165

CAS Journal Grade:3

Cited Count:

WoS CC Cited Count: 19

SCOPUS Cited Count: 16

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 0

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