FIELD: space engineering; aeronautical engineering; head fairings, jettisonable compartments, external tanks.
SUBSTANCE: proposed unit has first separable part coupled to second separable part over guide pins. Each part is provided with flanged tip which is engageable with holding members. Provision is made for clamping unit engageable with holding members with springs mounted between them; unit is provided with travel limiters and guide pins. Flanged tip of second separable part is provided with projection in which guide pins are secured, as well as perpendicular guide pins and adjustable travel limiters. Said projection is engageable with flanged tip of first separable part over parting plane. Clamping unit includes stud for connection of holding members and nut. Drive mechanism ensures release of nut at separation.
EFFECT: enhanced reliability of separation.
2 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LEVER-TYPE LOCK | 2004 |
|
RU2267450C2 |
| FLANGE POINT JOINT | 2008 |
|
RU2361790C1 |
| LEVER-TYPE LOCK | 2001 |
|
RU2212365C2 |
| UNIT OF ELECTRICAL CONNECTORS | 2005 |
|
RU2294039C1 |
| CARRIER ROCKET LARGE-SIZE DETACHABLE NOSE CONE | 2010 |
|
RU2424953C1 |
| PIPE CONNECTION | 2015 |
|
RU2594847C1 |
| SPACECRAFT MOVABLE STRUCTURAL ELEMENTS RETENTION DEVICE | 2018 |
|
RU2686804C1 |
| FLYING VEHICLE ELECTRICAL CONNECTOR UNIT | 2006 |
|
RU2320521C1 |
| DEVICE FOR CONNECTION AND DISCONNECTION OF ELECTRICAL CONNECTORS IN SEPARABLE COMPARTMENTS OF SPACECRAFT | 2004 |
|
RU2258643C1 |
| PROTECTIVE DEVICE FOR ON-BOARD PLATE OF DETACHABLE JOINT | 2004 |
|
RU2258642C1 |
