Effect of Thermo-Oxidative Ageing on Aviation Polysulfide Sealants

Aviation polysulfide sealants have been subjected to thermo-oxidative ageing. Their morphologies, Shore A hardness, and tensile properties have been tested by means of an optical microscope, a glossiness meter, a Shore A hardness meter, and a universal testing machine. Changes in their microstructur...

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Bibliographic Details
Published inApplied Mechanics and Materials Vol. 152-154; no. Mechanical Engineering and Materials; pp. 28 - 33
Main Authors Wang, Yun Ying, Meng, Jiang Yan
Format Journal Article
LanguageEnglish
Published Zurich Trans Tech Publications Ltd 01.01.2012
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Summary:Aviation polysulfide sealants have been subjected to thermo-oxidative ageing. Their morphologies, Shore A hardness, and tensile properties have been tested by means of an optical microscope, a glossiness meter, a Shore A hardness meter, and a universal testing machine. Changes in their microstructures were measured by Fourier-transform infrared spectroscopy and dynamic mechanical analysis (DMA). The results showed that glossiness was gradually reduced, and bubbles appeared on the surface of the samples during the course of ageing. The Shore A hardness of the sealant first decreased and then remained unchanged. Likewise, the tensile strength and tensile elongation percent first decreased and then remained unchanged. The infrared monitoring showed that the sealant underwent a post-cure reaction. The glass transition temperature and the room-temperature storage modulus of the sealant remained unchanged. No new functional groups were formed during ageing of the sealant. The aviation sealants did not undergo chemical degradation, showing that they have good endurance under thermo-oxidative conditions.
Bibliography:Selected, peer reviewed papers from the 2012 International Conference on Mechanical Engineering and Materials (ICMEM 2012), January 15-16, 2012, Melbourne, Australia
ObjectType-Article-2
SourceType-Scholarly Journals-1
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ISBN:9783037853528
3037853522
ISSN:1660-9336
1662-7482
1662-7482
DOI:10.4028/www.scientific.net/AMM.152-154.28