REVIEW OF FATIGUE LIFE EVALUATION FOR HELICOPTER COMPOSITE BLADES

Rotor blades are one of the most important parts of helicopter,and its can be used as lifting surface,pulling surface and control surface in flight. The fatigue life evaluation of rotor blades is the very important problem in helicopter engineering development. The history on fatigue life evaluation...

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Main Authors: MA CunWang, LI GuangLiang, QU BaoJie
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2019-01-01
Series:Jixie qiangdu
Subjects:
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.01.030
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author MA CunWang
LI GuangLiang
QU BaoJie
author_facet MA CunWang
LI GuangLiang
QU BaoJie
author_sort MA CunWang
collection DOAJ
description Rotor blades are one of the most important parts of helicopter,and its can be used as lifting surface,pulling surface and control surface in flight. The fatigue life evaluation of rotor blades is the very important problem in helicopter engineering development. The history on fatigue life evaluation for helicopter composite blades is simple reviewed in this paper.Then,the main methods of fatigue life evaluation for composite blades are introduced in detail,including to damage tolerance method,flaw tolerance method and its flow chart,practical application,key problems etc. Furthermore,aim to the practical engineering application,existing problems in the three methods are analysed in-depth. Next,the unconventionality fatigue life evaluation methods are introduced,including to residual strength method,progressive damage method,the method based on dynamic characteristic,and the examples of these methods are presented. At last,based on personal knowledge,the authors summarize some thinking to the fatigue life prediction for composite blades,and these thinking is perhaps helpful to related researcher.
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spelling doaj.art-825aa4a3b94c41ae9ad770f6a050a6132023-08-01T07:48:43ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692019-01-014118719530604102REVIEW OF FATIGUE LIFE EVALUATION FOR HELICOPTER COMPOSITE BLADESMA CunWangLI GuangLiangQU BaoJieRotor blades are one of the most important parts of helicopter,and its can be used as lifting surface,pulling surface and control surface in flight. The fatigue life evaluation of rotor blades is the very important problem in helicopter engineering development. The history on fatigue life evaluation for helicopter composite blades is simple reviewed in this paper.Then,the main methods of fatigue life evaluation for composite blades are introduced in detail,including to damage tolerance method,flaw tolerance method and its flow chart,practical application,key problems etc. Furthermore,aim to the practical engineering application,existing problems in the three methods are analysed in-depth. Next,the unconventionality fatigue life evaluation methods are introduced,including to residual strength method,progressive damage method,the method based on dynamic characteristic,and the examples of these methods are presented. At last,based on personal knowledge,the authors summarize some thinking to the fatigue life prediction for composite blades,and these thinking is perhaps helpful to related researcher.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.01.030Helicopter;Composite blades;Fatigue life evaluation;Review
spellingShingle MA CunWang
LI GuangLiang
QU BaoJie
REVIEW OF FATIGUE LIFE EVALUATION FOR HELICOPTER COMPOSITE BLADES
Jixie qiangdu
Helicopter;Composite blades;Fatigue life evaluation;Review
title REVIEW OF FATIGUE LIFE EVALUATION FOR HELICOPTER COMPOSITE BLADES
title_full REVIEW OF FATIGUE LIFE EVALUATION FOR HELICOPTER COMPOSITE BLADES
title_fullStr REVIEW OF FATIGUE LIFE EVALUATION FOR HELICOPTER COMPOSITE BLADES
title_full_unstemmed REVIEW OF FATIGUE LIFE EVALUATION FOR HELICOPTER COMPOSITE BLADES
title_short REVIEW OF FATIGUE LIFE EVALUATION FOR HELICOPTER COMPOSITE BLADES
title_sort review of fatigue life evaluation for helicopter composite blades
topic Helicopter;Composite blades;Fatigue life evaluation;Review
url http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.01.030
work_keys_str_mv AT macunwang reviewoffatiguelifeevaluationforhelicoptercompositeblades
AT liguangliang reviewoffatiguelifeevaluationforhelicoptercompositeblades
AT qubaojie reviewoffatiguelifeevaluationforhelicoptercompositeblades