Mechanical Properties of Silicone Elastomer Seals for Space Docking Vehicles

2018 2nd International Conference on Advanced Technologies in Design, Mechanical and Aeronautical Engineering

工业技术;机械制造;航空航天工程

Liao, C.H.J.^1 ; Lu, H.R.^1 ; Chang, X.H.^1 ; Sun, H.L.^1 ; Fan, S.H.Q.^1 ; Wu, H.L.^1

Beijing Institute of Astronautical Systems Engineering, Beijing, China^1

关键词: Design scheme;    Docking mechanisms;    Functional requirement;    Low impacts;    Sealing performance;    Silicone elastomers;    Space docking;    Space vehicles;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/408/1/012010/pdf
DOI  :  10.1088/1757-899X/408/1/012010

来源: IOP

【 摘 要 】

Low impact docking mechanisms (LIDM) are developing. The LIDM seal is one of the key components of the LIDM, and play very critical roles during the docking and berthing of space vehicles. Due to the severe functional requirements, it is difficult to develop the LIDM seal that is a silicone elastomer seal. The excellent mechanical property is firstly required for the LIDM seal. Five design schemes of the LIDM seal are proposed by this paper, and their mechanical properties are studied by the proposed finite element method. The mechanical properties of the LIDM seal have important impacts on the required sealing performance, docking feature and separation feature. The findings are beneficial for the development of the LIDM seal for space docking vehicles.