FIELD: the invention refers to cosmic technique and may be used for docking and dedocking of the mains of a flying apparatus and of a ground complex.
SUBSTANCE: the split block of the inner compartment of a flying apparatus has a with a drive mechanism and a tearing off plate with a casing fixed on it. They are fastened together with the aid of a collet lock. The collet lock has a collet with a band and a plunger with a ring lug. The collet is installed on the tearing off plate. The plunger is fulfilled with possibility of interacting of the tip with the collet's lobes. The ring lug of the plunger is fulfilled with a longitudinal groove. The unit has a bushing and rods. The bushing is fastened to the band of the collet, has a damper and a pin. The damper is installed with possibility of interacting with the tip of the plunger. The pin is installed with possibility of interacting with the mentioned longitudinal groove with the value equal to the value of interacting of the tip of the plunger with the lobes of the collet. The casing is not fulfilled hard and is provided with a flange. The flange has pins, limiters of displacement and a packing element. The pins are fulfilled with possibility of interacting with the body of the flying apparatus. The limiters of displacement are fulfilled with possibility of contacting with the lateral surface of the tearing off plate. The packing element is installed along the perimeter of the mentioned flange with possibility of interacting with the exterior surface of the body of the flying apparatus. The rods are fulfilled spring-like and are fixed with tearing off plate and the flange. The ring lug of the plunger is fulfilled with a spherical support surface interacting with the inner surface of the bushing.
EFFECT: increases reliability of the construction.
6 dwg
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Authors
Dates
2006-05-10—Published
2004-08-20—Filed