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Mechanical Modeling and Simulation for the Take-Off and Landing Performance Calculation of Low-Cost UAVs Read chapter Read first chapter

2022 | OriginalPaper | Chapter

Optimization of Design Method for Thermal Shrinkable Backup Ring in Aircraft Hydraulic Components

Authors : Xiangrong Xu, Yibo Ge, Changming Li

Published in: Proceedings of the 5th China Aeronautical Science and Technology Conference

Publisher: Springer Singapore

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Abstract

For the leakage failure caused by the damage of the rubber seal, the cause of the rubber ring damage is analyzed. Through the torsion and rapture of the rubber ring, the problem of thermal shrinkable poly tetrafluoroethylene (PTFE) backup ring heating over shrinkage is found. Finally, this failure is solved by optimizing the design method of the backup ring, including the reserved shrinkage, thickness compensation, etc.

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previous chapter Analysis and Improvement on Asymmetrical Wear in Aircraft Bootstrap Reservoir
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Metadata
Title
Optimization of Design Method for Thermal Shrinkable Backup Ring in Aircraft Hydraulic Components
Authors
Xiangrong Xu
Yibo Ge
Changming Li
Copyright Year
2022
Publisher
Springer Singapore
Book
Proceedings of the 5th China Aeronautical Science and Technology Conference

Print ISBN: 978-981-16-7422-8

Electronic ISBN: 978-981-16-7423-5

Copyright Year: 2022

DOI
https://doi.org/10.1007/978-981-16-7423-5_72

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