Manipulator for rocket recovery

A technology of manipulators and rockets, applied in the field of aerospace, can solve problems such as dumping, rocket landing deflection, explosion, etc., and achieve the effect of good mobility, low cost and simple structure

Pending Publication Date: 2019-03-08
YANSHAN UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In this way, when the rocket lands, it is prone to deflection, dumping, and even explosion

Method used

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  • Manipulator for rocket recovery
  • Manipulator for rocket recovery

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Embodiment Construction

[0020] In order to detail the technical content, structural features, achieved goals and effects of the present invention, the following will be described in detail in conjunction with the accompanying drawings.

[0021] Such as figure 1 As shown, it includes a claw 1, an arm 2, a landing platform 3, a small buffer hydraulic cylinder 4, a large buffer hydraulic cylinder 5, a driving hydraulic cylinder 6, a telescopic cantilever beam 7 and a telescopic support leg 8. The number of claws 1 is more than the number of arms 2. When each claw 1 is closed, it can form a complete cylinder. The height of the claw 1 is equal to the width of the arm 2. The end of the arm 2 is an arc-shaped cylinder with a diameter of The outer diameter of the arc is equal to that of the gripper 1. The gripper 1 and the arm 2 are fixedly connected one by one. The shape of the arm 2 is similar to a J shape. The first connection end of the lower end of the arm 2 is connected to the hinge seat of the bottom ...

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Abstract

The invention relates to a manipulator for rocket recovery. The manipulator is mainly used for the recovery of a first rocket stage. The manipulator structurally comprises a clamp, an arm, a landing platform, a large buffering hydraulic cylinder, a small buffering cylinder, a driving hydraulic cylinder, a telescopic suspension arm beam and a telescopic type supporting leg. The telescopic type suspension arm beam is fixedly connected with the telescopic type supporting leg, the telescopic type suspension arm beam and the driving hydraulic cylinder, the driving hydraulic cylinder and the arm, the arm and the bottom platform are connected through cylindrical pins, and the large buffering hydraulic cylinder and the small buffering cylinder are located on the bottom platform. When a rocket lands, the telescopic type suspension arm beam and the telescopic type supporting leg are turned into an opened state from a retracting state, the arm is driven to opened by the driving hydraulic cylinder, when the rocket lands on the landing platform, the arm is retracted by the moving of the driving hydraulic cylinder, and the landing buffering of the rocket is achieved. The buffering performance ofthe manipulator is excellent, the safety performance is high, the structure is simple, the cost is lower, the manipulator can be recycled, and automatic correcting of the rocket when the rocket landscan be achieved.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a manipulator for rocket recovery. Background technique [0002] The main purpose of studying the launch and recovery of reusable launch vehicles is to reduce launch costs. As we all know, the cost of space launch has always been high. The cost of transporting a 1kg object to the sky is about 10,000 to 20,000 US dollars, mainly because the launch vehicle is a one-time use. According to Pang Zhihao, an aerospace expert in my country, the successful recovery of the first stage of the launch vehicle can save 80% of the cost. [0003] The typical representative of overseas research on rocket recovery is the US Space Exploration Corporation (SpaceX). After four rocket recovery failures, it finally achieved a smooth landing of the recovered rocket. After the "Falcon 9" carrier rocket sent the cargo spacecraft into space, The first-stage rocket lands vertically on an offshore platf...

Claims

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Application Information

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IPC IPC(8): B64G5/00
CPCB64G5/00
Inventor 赵静一张亚卿闫振洋王留根任文斌
Owner YANSHAN UNIV
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