DocumentCode :
2353462
Title :
Analysis of movement and stability of the root lock mechanism of the space deployable mast
Author :
Liu, Heping ; Luo, Ani ; Zhang, Lixun
Author_Institution :
Harbin Eng. Univ., Harbin, China
fYear :
2010
fDate :
4-7 Aug. 2010
Firstpage :
1175
Lastpage :
1178
Abstract :
The root lock mechanism is a key component of the space deployable mast and influences the function of the mast directly. After analysis of the root lock mechanism, it is simplified as a kind of mechanism with two sliders and a spring. At first, when the mechanism carries out the lock actions, the vibration equation of the slider 2 is set up in the local coordinates, and then the displacement expression of the slider 2 is obtained in the whole coordinates by the coordinate transform. When the root lock mechanism is disturbed after the mast is locked, the vibration equation of the mechanism is set up. In the situation, stability of the root lock mechanism is analyzed, and relations and constraint conditions of the structural parameters are gotten. Actual values of these structural parameters are decided on further. Finally, numerical simulation is utilized to check up the movement of the root lock mechanism. After the analysis, selection of structural parameters is more reasonable and the design is more correct.
Keywords :
aerospace engineering; keys (locking); numerical analysis; springs (mechanical); supports; vibrations; coordinate transform; displacement expression; movement analysis; numerical simulation; root lock mechanism; sliders; space deployable mast; spring; stability analysis; structural parameters; vibration equation; Equations; Force; Frequency modulation; Mathematical model; Springs; Structural engineering; Vibrations;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation (ICMA), 2010 International Conference on
Conference_Location :
Xi´an
ISSN :
2152-7431
Print_ISBN :
978-1-4244-5140-1
Electronic_ISBN :
2152-7431
Type :
conf
DOI :
10.1109/ICMA.2010.5588167
Filename :
5588167
Link To Document :
بازگشت