FIELD: spacecraft handling equipment.
SUBSTANCE: proposed cross-piece contains carrying beam 1 with fitted on shackle 2. Balancing sockets 3 are made on carrying beam 1 in which slings with rigging units 5 for fastening spacecraft 6 are secured. Shackle 2 consists of eye and stem hinge connected with carrying beam 1. Stop is installed on stem below joint connecting stem with carrying beam 1 for engagement with locking socket made on carrying beam 1. Adjustable screw insert with lock is installed on shackle 2 between eye and stem. After fitting of cross-piece on hook, shackle is rigidly locked by stop relative to carrying beam to provided definite angle of tilting of spacecraft. Angle of tiling of lifted spacecraft 6 relative to horizontal plane is adjusted by changing length of adjustable screw insert of shackle.
EFFECT: provision of tolerable angle of tilting of spacecraft.
2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CROSS BAR FOR RELOCATING AND PERFORMING ASSEMBLING AND LINKING OPERATIONS OF LARGE SIZE ITEMS | 2006 |
|
RU2323870C1 |
| CROSS-BEAM | 2006 |
|
RU2329942C2 |
| CROSSARM | 2017 |
|
RU2703861C2 |
| CROSSBEAM | 2012 |
|
RU2526308C2 |
| CROSS BAR FOR DOCKING OF LARGE SPACE VEHICLE WITH CARRIER ROCKET EQUIPPED WITH SUPERCALIBER PAYLOAD FAIRING | 2007 |
|
RU2362724C2 |
| CHAIN SUSPENSION | 2012 |
|
RU2511761C1 |
| CROSSBAR | 2017 |
|
RU2661671C1 |
| CROSS ARM, CROSS ARM BEARING BEAM EQUALISING MECHANISM, CROSS ARM BEARING BEAM RIGGING; RIGGING LOAD LOCKING DEVICE, CROSS ARM BEARING BEAM SUPPORT FIXTURE, METHOD OF EQUILIBRIUM ADJUSTMENT OF CROSS ARM ON SUPPORT FIXTURES AND METHOD OF CROSS BEAM TRANSFER | 2008 |
|
RU2376237C1 |
| CROSS BEAM OF HORIZONTAL JOINT, CROSS BEAM BALANCING MECHANISM LOAD SETTER, CROSS BEAM BALANCING MECHANISM LOAD VECTOR COMPENSATION UNIT AND METHOD OF ADJUSTING CROSS BEAM BALANCING | 2008 |
|
RU2374164C1 |
| SUSPENSION FOR MOUNTING STRUCTURES | 0 |
|
SU660915A1 |
