A Configuration Synthesis Method of Deployable Mechanism Cells Used for Large Supporting Structures in Space

Chenhan Guang; Zilu Chen; Yang Yang

doi:10.1007/978-981-15-0142-5_16

A Configuration Synthesis Method of Deployable Mechanism Cells Used for Large Supporting Structures in Space

Chenhan Guang
, Zilu Chen
, Yang Yang^*

^*Corresponding author for this work

School of Mechanical Engineering and Automation

Beihang University

Research output: Contribution to journal › Article › peer-review

Abstract

More large payloads will be launched with the development of the aerospace industry, which means supporting structures for large payloads are also needed. Meanwhile, deployable supporting structures that can be synchronously packaged and deployed have been studied. However, if much larger or more complex structures are needed, building structures with identical deployable cells in space could be another choice. Therefore, we synthesize deployed configurations of deployable mechanism cells for large supporting structures in space with the help of finding the basic unit for a certain three-dimensional array. Then we present several examples of deployable mechanism cells based on the synthesized deployed configurations.

Original language	English
Pages (from-to)	152-160
Number of pages	9
Journal	Mechanisms and Machine Science
Volume	79
DOIs	https://doi.org/10.1007/978-981-15-0142-5_16
State	Published - 2020

Keywords

Configuration synthesis method
Deployable mechanism cells
Large supporting structures

Access to Document

10.1007/978-981-15-0142-5_16

Cite this

@article{807fe5a1866a48b6ac9b1a1478b06685,

title = "A Configuration Synthesis Method of Deployable Mechanism Cells Used for Large Supporting Structures in Space",

abstract = "More large payloads will be launched with the development of the aerospace industry, which means supporting structures for large payloads are also needed. Meanwhile, deployable supporting structures that can be synchronously packaged and deployed have been studied. However, if much larger or more complex structures are needed, building structures with identical deployable cells in space could be another choice. Therefore, we synthesize deployed configurations of deployable mechanism cells for large supporting structures in space with the help of finding the basic unit for a certain three-dimensional array. Then we present several examples of deployable mechanism cells based on the synthesized deployed configurations.",

keywords = "Configuration synthesis method, Deployable mechanism cells, Large supporting structures",

author = "Chenhan Guang and Zilu Chen and Yang Yang",

note = "Publisher Copyright: {\textcopyright} 2020, Springer Nature Singapore Pte Ltd.",

year = "2020",

doi = "10.1007/978-981-15-0142-5\_16",

language = "英语",

volume = "79",

pages = "152--160",

journal = "Mechanisms and Machine Science",

issn = "2211-0984",

publisher = "Springer Netherlands",

}

TY - JOUR

T1 - A Configuration Synthesis Method of Deployable Mechanism Cells Used for Large Supporting Structures in Space

AU - Guang, Chenhan

AU - Chen, Zilu

AU - Yang, Yang

PY - 2020

Y1 - 2020

N2 - More large payloads will be launched with the development of the aerospace industry, which means supporting structures for large payloads are also needed. Meanwhile, deployable supporting structures that can be synchronously packaged and deployed have been studied. However, if much larger or more complex structures are needed, building structures with identical deployable cells in space could be another choice. Therefore, we synthesize deployed configurations of deployable mechanism cells for large supporting structures in space with the help of finding the basic unit for a certain three-dimensional array. Then we present several examples of deployable mechanism cells based on the synthesized deployed configurations.

AB - More large payloads will be launched with the development of the aerospace industry, which means supporting structures for large payloads are also needed. Meanwhile, deployable supporting structures that can be synchronously packaged and deployed have been studied. However, if much larger or more complex structures are needed, building structures with identical deployable cells in space could be another choice. Therefore, we synthesize deployed configurations of deployable mechanism cells for large supporting structures in space with the help of finding the basic unit for a certain three-dimensional array. Then we present several examples of deployable mechanism cells based on the synthesized deployed configurations.

KW - Configuration synthesis method

KW - Deployable mechanism cells

KW - Large supporting structures

UR - https://www.scopus.com/pages/publications/85072795207

U2 - 10.1007/978-981-15-0142-5_16

DO - 10.1007/978-981-15-0142-5_16

M3 - 文章

AN - SCOPUS:85072795207

SN - 2211-0984

VL - 79

SP - 152

EP - 160

JO - Mechanisms and Machine Science

JF - Mechanisms and Machine Science

ER -

A Configuration Synthesis Method of Deployable Mechanism Cells Used for Large Supporting Structures in Space

Abstract

Keywords

Access to Document

Other files and links

Fingerprint

Cite this