2010
DOI: 10.1179/175158310x481745
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Two body abrasive wear and frictional characteristics of sealing elastomers under unidirectional lubricated sliding conditions

Abstract: Since abrasion is a common cause of seal failures, understanding the mechanisms of abrasion of an elastomer in the presence of lubricants is of importance in sealing applications. In this research a block on ring configuration was used to study the influence of lubrication on the two body abrasion of several commonly used sealing elastomers (two acrylonitrile butadiene rubbers, an acrylic rubber and a fluoro rubber). The friction force and the abrasive wear of the samples were measured and the worn surfaces an… Show more

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Cited by 8 publications
(3 citation statements)
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“…This makes the O-ring to wear much faster than in a device that uses a conventional hydraulic oil [16]. Moreover, the fluid leakage caused by high friction loss between the sealing pairs limits the usage life and the performance of MR equipment [17]. To sum up, although the movement pattern of the MR damper is not much different from the traditional hydraulic cylinder, there is a great difference in wear mechanism between the sealing pairs.…”
Section: Introductionmentioning
confidence: 99%
“…This makes the O-ring to wear much faster than in a device that uses a conventional hydraulic oil [16]. Moreover, the fluid leakage caused by high friction loss between the sealing pairs limits the usage life and the performance of MR equipment [17]. To sum up, although the movement pattern of the MR damper is not much different from the traditional hydraulic cylinder, there is a great difference in wear mechanism between the sealing pairs.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, whether the landing gear lock mechanism can work normally is directly related to the safety of the aircraft [2], which is an important part of the landing gear design. During the use of the landing gear, the lock mechanism will gradually wear during the unlocking and locking process, resulting in the change of unlocking force [3]. If the unlocking force is abnormal, it will lead to the landing gear retraction failure, which will threaten the safety of aircraft takeoff and landing [4,5].…”
Section: Introductionmentioning
confidence: 99%
“…3 If the wear is within the specified range, the lock mechanism can maintain normal working conditions. If it exceeds the upper limit of wear, the friction force of the friction pair formed by the lock mechanism will rise sharply, 4 resulting in a retractable failure of the landing gear. 5 The wear problem has been studied at home and abroad for a long time.…”
Section: Introductionmentioning
confidence: 99%