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A kind of multi-functional rocket transportation vertical vehicle

A transport vehicle and multi-functional technology, applied in the field of booster rocket transportation and erection vehicles, can solve the problems of difficulty in on-site command and coordination, low operation efficiency, and complicated docking operations, and achieve easy connection operations, high automation efficiency, and elimination of additional The effect of bending moment

Active Publication Date: 2021-05-07
NO 63921 UNIT OF PLA +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] At present, the docking operation of domestic booster rockets and core-stage rockets is complicated, with low standardization and automation, high requirements for operators’ skills, and difficulty in on-site command and coordination. Practical problems such as low efficiency, long time of occupying the launch station, and the lifting link is easily affected by wind
With the intensification of competition in the domestic and foreign launch vehicle markets, the disadvantages of the existing booster rocket and core stage rocket docking methods have gradually emerged, which can no longer meet the requirements of commercial operation

Method used

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  • A kind of multi-functional rocket transportation vertical vehicle
  • A kind of multi-functional rocket transportation vertical vehicle
  • A kind of multi-functional rocket transportation vertical vehicle

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Embodiment Construction

[0031] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0032] as attached figure 1 As shown, the present invention provides a multifunctional rocket transportation erecting vehicle, which comprises a transport vehicle 1, a lifting adjustment device 2, an arm adjustment device 3, a vertical arm 4, a vertical oil cylinder 5, and legs 6 and lifting system 7;

[0033] One end of the vertical arm is hinged to the tail of the transport vehicle, and the other end of the vertical arm is installed with a lifting adjustment device. The lifting adjustment device is fixedly connected with the head of the booster rocket. Height adjustment in the horizontal, vertical and vertical directions; the arm arm adjustment device is installed on the vertical arm to realize the locking and release of the booster rocket, and the arm arm adjustment device can realize horizontal, vertical and vertical three directions at the same time....

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Abstract

The invention discloses a multifunctional rocket transport erector, which belongs to the technical field of ground transport launching devices for launch vehicles. One end of the vertical arm is hinged to the tail of the transport vehicle, and the other end of the vertical arm is installed with a lifting adjustment device. The lifting adjustment device realizes the horizontal, vertical and vertical height adjustment of the booster rocket in the horizontal plane after the vertical arm is erected. ;The arm-holding adjustment device is installed on the vertical arm to realize the locking and loosening of the booster rocket, and the arm-holding adjustment device can realize horizontal, vertical and vertical adjustment at the same time; the vertical oil cylinder is installed on the transport vehicle and the lifter Between the vertical arms, the erection and recovery of the vertical arm are realized; the outriggers are installed at the bottom of the transport vehicle to support the balance of the transport vehicle when the booster rocket is erected. The erecting vehicle of the present invention is suitable for booster rockets in bundled rockets, can transport and transfer the booster rockets, erect them as a whole after arriving at the launch area, and complete rapid docking with the core rocket.

Description

technical field [0001] The invention relates to the technical field of aerospace ground support equipment, in particular to a booster rocket transportation erector. Background technique [0002] The bundled rocket is mainly composed of a core rocket bundled with multiple booster rockets, which has the advantages of high thrust, high initial velocity, and low cost. [0003] The common docking method of the booster rocket and the core rocket of the bundled rocket in my country is: the booster rocket is hoisted to the transport vehicle by driving in the technical area, and the transport vehicle transports the booster rocket to the launch area to realize the transition operation; After entering the launch area, the tower crane or other cranes on the launch tower and the operators cooperate to lift the booster rocket from the transport vehicle, and gradually turn it from a horizontal state to a vertical state, and then adjust the booster rocket by the lifting equipment. The space ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B66C23/36B66C23/38B66C23/62B60P3/00
CPCB60P3/00B66C23/36B66C23/38B66C23/62
Inventor 王晓明宋道宏张志成周军波唐小松任刚李苏疆邹阳侯绪超谭波杨兴胡飘
Owner NO 63921 UNIT OF PLA
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