FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, and more specifically to operation of optoelectronic equipment. Spacecraft light-shielding device cover assembly comprises a frame, a cover, a hinged-and-leverage mechanism of a movable connection, spring compensators. Besides, assembly includes two fixation mechanisms, end position sensor and limiters stops. Hinged-leverage mechanism of movable connection is made in form of double crank-and-rocker mechanism. Cranks interact with L-shaped connecting rods. In closed and open positions of leaflets hinges of crankshafts, connecting rods and yokes are located on one straight line of "zero" line. Limit stops thrusts are installed with a gap to cranks when the latter turn beyond the "zero" line by 3° in extreme positions. Compensators are installed on the frame and interact with the flaps only in their closed position.
EFFECT: enabling higher reliability.
1 cl, 8 dwg
Title | Year | Author | Number |
---|---|---|---|
SPACECRAFT LIGHT PROTECTION DEVICE | 2009 |
|
RU2391264C1 |
LIGHT PROTECTIVE DEVICE FOR SPACE VEHICLE | 1995 |
|
RU2094336C1 |
LIGHT SHIELD FOR SPACECRAFT | 1997 |
|
RU2128134C1 |
SPACECRAFT LIGHT PROTECTION DEVICE COVER ASSEMBLY | 2012 |
|
RU2514015C1 |
RETAINER FOR SEALED CONTAINER WITH RESEARCH HARDWARE | 2013 |
|
RU2538649C1 |
COVER UNIT OF THE AIRCRAFT VISUAL OPTICAL SYSTEM | 2015 |
|
RU2624973C2 |
SPACE VEHICLE LIGHT PROTECTION DEVICE | 1994 |
|
RU2089467C1 |
CONTROL DRIVE OF THE PLUG DOOR OF THE VEHICLE | 2022 |
|
RU2792906C1 |
DRIVE DEVICE OF TWO-LEAF DOOR | 2021 |
|
RU2784881C2 |
DEVICE FOR OPENING AND CLOSING DOOR LEAVES OF ELEVATOR CAGE | 1999 |
|
RU2175304C2 |
Authors
Dates
2021-03-02—Published
2020-05-21—Filed