FIELD: mechanical engineering.
SUBSTANCE: invention relates to the field of mechanical engineering, in particular to devices for fixing a multi-section structure of a spacecraft. The device consists of harmonically folded sections pivotally connected to each other and to the spacecraft through the first section. On one of the sections there is a fixing element made in the form of a hinged rigid hook equipped with a spring. On the other section, adjacent to the first one, the axis is pivotally fixed. The axis is installed in the rocker, with the possibility of interaction with the inner side of the hook. The axis is equipped with a spring that allows it to be deflected by the hook.
EFFECT: increased reliability of fixation.
3 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
SPACECRAFT SOLAR PANEL | 2015 |
|
RU2619158C2 |
DEVICE FOR DEPLOYMENT OF MULTI-SECTION STRUCTURES | 2022 |
|
RU2809497C1 |
SPACECRAFT TRANSFORMABLE STRUCTURE SECTION RETENTION DEVICE | 2024 |
|
RU2826959C1 |
DEVICE FOR OPENING STRUCTURAL ELEMENTS | 2019 |
|
RU2729925C1 |
SOLAR BATTERY (VERSIONS) | 2004 |
|
RU2258640C1 |
DEVICE FOR FIXING A HINGED JOINT | 2017 |
|
RU2657811C1 |
METHOD OF OPENING MULTI-SECTION STRUCTURES | 2019 |
|
RU2729872C1 |
MULTILINK ROD FOR SPACECRAFT SOLAR BATTERY | 2020 |
|
RU2745126C1 |
SOLAR PANEL ON FLEXIBLE SUBSTRATE AND METHOD FOR OPENING THEREOF | 2014 |
|
RU2574057C2 |
SOLAR BATTERY MECHANICAL DEVICE CONSTRUCTION MANUFACTURING METHOD | 2018 |
|
RU2729866C2 |
Authors
Dates
2022-04-07—Published
2021-12-13—Filed