-
- Mollon Guilhem
- University of Lyon, CNRS LaMCoS, INSA Lyon, UMR 5259
-
- Kounoudji Komla Apélété
- University of Lyon, CNRS LaMCoS, INSA Lyon, UMR 5259
-
- Renouf Mathieu
- University of Montpellier, CNRS LMGC, UMR 5508
-
- Berthier Yves
- University of Lyon, CNRS LaMCoS, INSA Lyon, UMR 5259
書誌事項
- 公開日
- 2016
- DOI
-
- 10.2474/trol.11.255
- 公開者
- 一般社団法人 日本トライボロジー学会
この論文をさがす
説明
An experimental approach was adopted to understand service damages such as crack initiation and surface degradation of bolted joints used in the junction technology of aircraft air bleed valve systems. A vibratory testing stage combined to Digital Image Correlation (DIC) focus on an experimental model device of valve body/actuator body junction. DIC coupled with in situ tribological observations and a Finite Element Model (FEM) has been used to identify more clearly local contact conditions. This approach has enlightened peeling-off and micro-slips instabilities under vibratory loadings, leading to third body formation in bolted joints contacts. The morphology of such third body is placed at the focus of damages observed in involved air bleed valve systems.
収録刊行物
-
- Tribology Online
-
Tribology Online 11 (2), 255-263, 2016
一般社団法人 日本トライボロジー学会
- Tweet
詳細情報 詳細情報について
-
- CRID
- 1390282680245700992
-
- NII論文ID
- 130005149906
-
- ISSN
- 18812198
- 1881218X
-
- 本文言語コード
- en
-
- データソース種別
-
- JaLC
- Crossref
- CiNii Articles
-
- 抄録ライセンスフラグ
- 使用不可
