FIELD: transport.
SUBSTANCE: invention relates to machine building, in particular for rocket transportation on carrier support. Shock-absorbing pad for rocket fastening on carrier support during its transportation contains suction cups with seals at its both sides, channels of suction cups connection, where suction cup chamber at one side of pad is divided by resilient diaphragm into two chambers each one of which includes channel with tap the valve of which serves for disconnecting or connecting with trunk channel of preliminary or constant air vacuum pressure. The pad also is provided with air vacuum pressure distribution system to deliver air vacuum pressure to trunk channels and with pressure gauge and is made with possibility to mate nonplanar surfaces of support and rocket.
EFFECT: invention allows to control condition of rocket fastening on carrying support during transportation.
4 cl, 2 dwg
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ROCKET FASTENING AT CARRIER SUPPORT WITH HELP OF PAD WITH SUCTION CUPS | 2012 |
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Authors
Dates
2014-12-10—Published
2012-12-18—Filed