FIELD: mechanical engineering; device for withdrawal of service lines from sides of rocket, ship, etc. SUBSTANCE: device has boom which is articulated on base and is made in form of movable door 1 of protective structure 2; carriage 5 connected with drive is mounted in guide 3 by means of rollers 4; carriage 5 bears detachable joint 10. balancing unit is made in form of spring suspension articulated with carriage and protective structure. Movable door is linked with protective structure by means of articulated rod fitted units for locking the door in the closed and open positions and unit for unlocking the door open position. For bringing the service lines to side of launch vehicle, drive 6 is provided which turns door 3 and shifts carriage 5 over its guides, thus bringing the service lines to detachable joint. EFFECT: enhanced reliability. 2 dwg
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Authors
Dates
2001-11-20—Published
1999-07-19—Filed