Research on Fatigue Fracture Kinetics of Helicopter Fuselage Bolting Elements

被引：0
|
作者：
Urbahs, A. [1 ]
Carjova, K. [1 ]
Nasibullins, A. [2 ]
Fescuks, J. [1 ]
机构：
[1] Riga Tech Univ, Inst Aeronaut, Lomonosova 1A,K-1, Riga, Latvia
[2] Aviatest LTD, 1 Rezeknes St, Riga, Latvia
来源：
PROCEEDINGS OF THE 20TH INTERNATIONAL SCIENTIFIC CONFERENCE TRANSPORT MEANS 2016 | 2016年
关键词：
fatigue cracks; Acoustic Emission testing; helicopter structure; bolts; fractographic research;
D O I：
暂无
中图分类号：
U [交通运输];
学科分类号：
08 ; 0823 ;
摘要：
The paper contains results of experimental research carried out helicopter bench. Helicopter test bench was used to develop defect localization methodology of helicopter structure fatigue damage technical diagnostics. Analysing helicopter structural defects for different helicopters types it is concluded that the joint elements of helicopter tail boom are still exposed to fatigue crack formation, crack development process is not controlled, and sometimes it is not possible to detect defects at all.
引用
收藏
页码：1040 / 1044
页数：5
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