Failure damage evolution of a mechanical joint of carbon fiber metal laminates under the bearing failure mode

Terutake Matsubara, Yoshihiro Takao, Wen Xue Wang

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Glass fiber-reinforced metal laminates have already been developed as Glare and used in A380 as upper fuselage panels. Though a lot of efforts were made to develop Carbon Fiber-reinforced Metal Laminates (CFMLs), two major problems were unsolved. They were the galvanic corrosion and large thermal residual stresses. A new galvanic corrosion-resistant coating has successfully proposed, which consists of a sulfuric acid anodizing and a silica nano-particle reinforced hybrid sol-gel coating. This paper investigates the damage evolution of a mechanical pin joint of CFML with the new coating under the quasi-static tensile loading. Two peaks of load and their damage evolutions are identified by the microscopic fracture analysis.

Original languageEnglish
Title of host publicationProgress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008
Pages188-191
Number of pages4
Publication statusPublished - Dec 1 2008
Event6th Asian-Australasian Conference on Composite Materials: Progress of Composites 2008 in Asia and Australasia, ACCM 2008 - Kumamoto, Kyushu, Japan
Duration: Sep 23 2008Sep 26 2008

Publication series

NameProgress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008

Other

Other6th Asian-Australasian Conference on Composite Materials: Progress of Composites 2008 in Asia and Australasia, ACCM 2008
CountryJapan
CityKumamoto, Kyushu
Period9/23/089/26/08

Fingerprint

Bearings (structural)
Fiber reinforced metals
Failure modes
Carbon fibers
Laminates
Metals
Coatings
Corrosion
Glare
Fuselages
Anodic oxidation
Sulfuric acid
Thermal stress
Silicon Dioxide
Glass fibers
Particles (particulate matter)
Sol-gels
Residual stresses
Silica
carbon fiber

All Science Journal Classification (ASJC) codes

  • Ceramics and Composites

Cite this

Matsubara, T., Takao, Y., & Wang, W. X. (2008). Failure damage evolution of a mechanical joint of carbon fiber metal laminates under the bearing failure mode. In Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008 (pp. 188-191). (Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008).

Failure damage evolution of a mechanical joint of carbon fiber metal laminates under the bearing failure mode. / Matsubara, Terutake; Takao, Yoshihiro; Wang, Wen Xue.

Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008. 2008. p. 188-191 (Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Matsubara, T, Takao, Y & Wang, WX 2008, Failure damage evolution of a mechanical joint of carbon fiber metal laminates under the bearing failure mode. in Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008. Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008, pp. 188-191, 6th Asian-Australasian Conference on Composite Materials: Progress of Composites 2008 in Asia and Australasia, ACCM 2008, Kumamoto, Kyushu, Japan, 9/23/08.
Matsubara T, Takao Y, Wang WX. Failure damage evolution of a mechanical joint of carbon fiber metal laminates under the bearing failure mode. In Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008. 2008. p. 188-191. (Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008).
Matsubara, Terutake ; Takao, Yoshihiro ; Wang, Wen Xue. / Failure damage evolution of a mechanical joint of carbon fiber metal laminates under the bearing failure mode. Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008. 2008. pp. 188-191 (Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008).
@inproceedings{636997d07cb34481b6d0f9aef37a6805,
title = "Failure damage evolution of a mechanical joint of carbon fiber metal laminates under the bearing failure mode",
abstract = "Glass fiber-reinforced metal laminates have already been developed as Glare and used in A380 as upper fuselage panels. Though a lot of efforts were made to develop Carbon Fiber-reinforced Metal Laminates (CFMLs), two major problems were unsolved. They were the galvanic corrosion and large thermal residual stresses. A new galvanic corrosion-resistant coating has successfully proposed, which consists of a sulfuric acid anodizing and a silica nano-particle reinforced hybrid sol-gel coating. This paper investigates the damage evolution of a mechanical pin joint of CFML with the new coating under the quasi-static tensile loading. Two peaks of load and their damage evolutions are identified by the microscopic fracture analysis.",
author = "Terutake Matsubara and Yoshihiro Takao and Wang, {Wen Xue}",
year = "2008",
month = "12",
day = "1",
language = "English",
isbn = "9784901381321",
series = "Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008",
pages = "188--191",
booktitle = "Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008",

}

TY - GEN

T1 - Failure damage evolution of a mechanical joint of carbon fiber metal laminates under the bearing failure mode

AU - Matsubara, Terutake

AU - Takao, Yoshihiro

AU - Wang, Wen Xue

PY - 2008/12/1

Y1 - 2008/12/1

N2 - Glass fiber-reinforced metal laminates have already been developed as Glare and used in A380 as upper fuselage panels. Though a lot of efforts were made to develop Carbon Fiber-reinforced Metal Laminates (CFMLs), two major problems were unsolved. They were the galvanic corrosion and large thermal residual stresses. A new galvanic corrosion-resistant coating has successfully proposed, which consists of a sulfuric acid anodizing and a silica nano-particle reinforced hybrid sol-gel coating. This paper investigates the damage evolution of a mechanical pin joint of CFML with the new coating under the quasi-static tensile loading. Two peaks of load and their damage evolutions are identified by the microscopic fracture analysis.

AB - Glass fiber-reinforced metal laminates have already been developed as Glare and used in A380 as upper fuselage panels. Though a lot of efforts were made to develop Carbon Fiber-reinforced Metal Laminates (CFMLs), two major problems were unsolved. They were the galvanic corrosion and large thermal residual stresses. A new galvanic corrosion-resistant coating has successfully proposed, which consists of a sulfuric acid anodizing and a silica nano-particle reinforced hybrid sol-gel coating. This paper investigates the damage evolution of a mechanical pin joint of CFML with the new coating under the quasi-static tensile loading. Two peaks of load and their damage evolutions are identified by the microscopic fracture analysis.

UR - http://www.scopus.com/inward/record.url?scp=84887507444&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84887507444&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84887507444

SN - 9784901381321

T3 - Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008

SP - 188

EP - 191

BT - Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008

ER -