FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, particularly, to tensioning assemblies. Tensioning assembly comprises a platform with cables fixed between said strap and first bracket, and second and third brackets for mounting on housing inner and outer sides. Bracket shape is selected to exclude their movement relative to structural housing. First bracket is connected to the third bracket by means of a tension adjustment mechanism consisting of two axes, a hinge, a pull rod, a pin, a washer and a nut.
EFFECT: uniform tension of the cables.
6 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
SLINGS TENSION ADJUSTMENT ASSEMBLY | 2018 |
|
RU2691552C1 |
METHOD FOR ASSEMBLING XENON HIGH PRESSURE TANK WITH CABLE FASTENING SYSTEM | 2022 |
|
RU2793771C1 |
PANEL TENSIONING ASSEMBLY | 2022 |
|
RU2790106C1 |
ADJUSTABLE CONSTUCTION ATTACHING LUG WITH INTERFACE ON SLINGS | 2015 |
|
RU2625211C2 |
UNIVERSAL MOUNTING INTERFACE FOR INTERROJUSTATION OF EQUIPMENT WITH CABLE FASTENING SYSTEM | 2018 |
|
RU2689892C1 |
ADJUSTABLE SECURING ASSEMBLY | 2013 |
|
RU2559370C2 |
ADJUSTABLE CLAMPING UNIT | 2016 |
|
RU2646041C2 |
ADJUSTMENT CONNECTING DEVICE | 2014 |
|
RU2605666C2 |
ASSEMBLY FOR DOCKING OF SPACECRAFT LOAD CARRYING STRUCTURE (VERSIONS) | 2019 |
|
RU2729909C1 |
REINFORCEMENT UNIT FOR FRAME OF FORCE LATTICE CONSTRUCTION OF HOUSING FROM POLYMER COMPOSITE MATERIALS (VERSIONS) | 2019 |
|
RU2733309C1 |
Authors
Dates
2020-01-30—Published
2019-03-27—Filed