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Automatic docking device and method for right angle coordinate flexibility non-contact type connector

An automatic docking and non-contact technology, applied in aircraft, motor vehicles, transportation and packaging, etc., can solve the problems of difficult manual docking of connectors, high labor intensity, poor safety, etc., and achieve simple structure, high degree of automation, The effect of adaptability

Active Publication Date: 2019-06-18
BEIJING INST OF SPACE LAUNCH TECH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to solve the problems of difficult manual docking, high labor intensity, low efficiency and poor safety of connectors in the fields of launch vehicle launch system and LNG ship unloading system, the invention provides an automatic docking device for rectangular coordinate flexible non-contact connectors And a docking method, which has the advantages of high degree of automation, strong adaptability, simple structure, safety and reliability

Method used

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  • Automatic docking device and method for right angle coordinate flexibility non-contact type connector
  • Automatic docking device and method for right angle coordinate flexibility non-contact type connector
  • Automatic docking device and method for right angle coordinate flexibility non-contact type connector

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Embodiment Construction

[0031] Such as Figure 1-4 As shown, a Cartesian coordinate flexible non-contact connector automatic docking device of the present invention includes a base 1, an advance and retreat seat 2, a traverse seat 3, a lifting seat 4, a flexible clamping propulsion mechanism 5, a non-contact detection system 6 and a connector Component7.

[0032] The base 1 includes a base frame 1-1, and the upper and rear ends of the base frame 1-1 are equipped with an advancing and retreating AC servo motor 1-2, a double output shaft reducer 1-3 and two pair of right angle reducers 1-5. Two advance and retreat guide rail pairs 1-6 and support bases 1-8 are installed on the top of the base frame 1-1. 8 on. The forward and backward AC servo motor 1-2 is connected with the forward and backward screw pair 1-7 through the double output shaft reducer 1-3, the transmission shaft 1-4, the right angle reducer 1-5, and the forward and backward AC servo motor 1-2 drives Advance and retreat lead screw pair ...

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Abstract

The invention relates to an automatic docking device and method for a right angle coordinate flexibility non-contact type connector used for space launch technology and in the transportation process of liquefied natural gas (LNG). The invention aims at providing the docking device and method for the connector, which have the advantages of high automation degree, strong adaptive capacity, simple structure, safety, reliability and the like. The automatic docking device for the right angle coordinate flexibility non-contact type connector comprises a pedestal, an advancing and retreating seat, atransverse movement seat, a lifting seat, a flexible clamping propulsion mechanism, a non-contact detection system and a connector component, wherein the advancing and retreating seat is installed above the pedestal, the transverse movement seat is installed above the advancing and retreating seat, the lifting seat is installed above the transverse movement seat, the flexible clamping propulsion mechanism is installed above the lifting seat, the non-contact detection system comprises a target plate and a non-contact sensor, the non-contact sensor is installed on the lifting seat, and the target plate is installed on a surface of a storage box; and the connector component comprises a connector, and the connector is used for connecting with an interface.

Description

technical field [0001] The invention relates to an automatic docking device and method for a Cartesian coordinate flexible non-contact connector used in space launch technology and liquefied natural gas (LNG) transportation. Background technique [0002] In the fields of space vehicle launch system, liquefied natural gas (LNG) unloading system, etc., the ground propellant delivery pipeline, the interface between the unloading arm and the rocket storage tank, and the interface between the LNG carrier storage tank need to be connected through connectors to realize Propellant, LNG transfer or discharge rocket storage tanks, transport ship storage tanks. At present, the connection between the connector and the interface of the rocket tank and the interface of the LNG carrier tank generally needs to be completed by manual operation, and the interface of the rocket tank and the interface of the LNG carrier tank are in multiple places in space under the action of external wind load...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/00B64G5/00B63B27/24
Inventor 李泳峄翟旺吴新跃白文龙
Owner BEIJING INST OF SPACE LAUNCH TECH
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