FIELD: aviation.
SUBSTANCE: mechanism of sealing of joint of docking units contains docking frames with systems of locks with passive hooks and active hooks on eccentric shafts with pulleys with teeth, electric drives, end face sealing on a frame, rods in the form of gear wheel segments with cylindrical elements at end faces and end face teeth for connection of pulleys and a drive output shaft, locks, couplers in the form of a rod with spherical elements on end faces and cap nuts for connection of gear wheel segments. The number of gear wheel segments is equal to number of locks.
EFFECT: invention allows to improve reliability of connection between pulleys of locks and an electric drive and to avoid the break of drafts.
7 dwg
Title | Year | Author | Number |
---|---|---|---|
SEALING MECHANISM OF JOINT OF DOCKING UNITS | 2019 |
|
RU2717287C1 |
SEALING MECHANISM OF THE JOINT OF THE DOCKING ASSEMBLY OF SPACECRAFT | 2016 |
|
RU2648662C2 |
HATCH COVER OPENER | 2010 |
|
RU2428360C1 |
PAYLOAD SEPARATION SYSTEM | 2009 |
|
RU2396191C1 |
UNCOUPLING DEVICE | 2013 |
|
RU2543477C2 |
UNCOUPLING DEVICE | 2013 |
|
RU2545134C2 |
ANDROGYNOUS DOCKING UNIT FOR SPACECRAFT BASED ON OPEN MODULAR ARCHITECTURE | 2022 |
|
RU2802572C1 |
SPACECRAFT ANDROGENIC DOCKING UNIT | 2005 |
|
RU2291821C1 |
PASSIVE DOCKING ASSEMBLY | 2007 |
|
RU2349517C1 |
CLAMP | 2003 |
|
RU2243082C2 |
Authors
Dates
2015-08-10—Published
2014-01-09—Filed