[1]黄 钺,顿向明,山 磊.运载火箭自动加注机器人结构设计及有限元分析[J].机械与电子,2021,(01):76-80.
 HUANG Yue,DUN Xiangming,SHAN Lei.Structure Design and Finite Element Analysis of Automatic Filling Robot for Launch Vehicle[J].Machinery & Electronics,2021,(01):76-80.
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运载火箭自动加注机器人结构设计及有限元分析()
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机械与电子[ISSN:1001-2257/CN:52-1052/TH]

卷:
期数:
2021年01期
页码:
76-80
栏目:
智能工程
出版日期:
2021-01-20

文章信息/Info

Title:
Structure Design and Finite Element Analysis of Automatic Filling Robot for Launch Vehicle
文章编号:
1001-2257(2021)01-0076-05
作者:
黄 钺1顿向明2 山 磊3
1.上海交通大学机械与动力工程学院,上海 200240;
2.上海交通大学航空与航天学院,上海 200240;
3.常州远量机器人技术有限公司,江苏 常州 213164
Author(s):
HUANG Yue1 DUN Xiangming2 SHAN Lei3
1 .School of Mechanical Engineering , Shanghai Jiao Tong University , Shanghai 200240, China;
2 School of Aeronautics and Astronautics , Shanghai Jiao Tong University, Shanghai 200240 , China;
3 Changzhou Yuanliang Robot Technology Co., Ltd, Changzhou 213164, China
关键词:
加注机器人管道机械臂SolidWorks Simulation有限元
Keywords:
filling robot pipeline manipulator SolidWorks Simulation finite element
分类号:
TH122; TP242
文献标志码:
A
摘要:
针对运载火箭推进剂加注自动化过程的实现,设计了一种能够与箭体连接头自动对接与脱离的加注机器人。该机器人以管道机械臂作为机器人本体,配合激光雷达实现自动定位与跟踪。机械臂既是机器人定位跟踪的载体也是推进剂加注管道,加泄连接器安装在机械臂末端,作为与箭体连接头对接的机械载体。利用建模软件建立机器人三维实体模型,将模型简化后导入SolidWorks Simulation进行有限元分析,得到了其应力云图以及变形位移图,通过分析验证了机构设计的可靠性和合理性。
Abstract:
Aiming at the realization of the automatic process of launch vehicle propellant filling, a filling robot that can automatically dock and disconnect with the rocket body connector is designed. The robot uses the pipeline manipulator as the robot body, and cooperates with the laser radar to realize automatic positioning and tracking. The robotic arm is not only a carrier for the positioning and tracking of the robot but also a propellant filling pipe. The fill-drain connector is installed at the end of the robotic arm as a mechanical carrier for docking with the rocket body connector. The 3D solid model of the robot was established using modeling software, and the model was simplified and imported into SolidWorks Simulation for finite element analysis, and its stress cloud diagram and deformation displacement diagram were obtained. The reliability and rationality of the mechanism design were verified through analysis.

参考文献/References:

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[3] 闻靖,顿向明,张育林,等.推进剂加注自动对接与脱离机器人技术现状与发展趋势研究[J].机器人技术与应用,2010(6):20-23.

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[6] 游嘉伟,顿向明,山磊,等.运载火箭推进剂加注机器人机构设计[J].机电一体化,2016(4):41-44.

[7] 黄小妮, 顿向明,张育林,等.运载火箭推进剂加注自动对接与脱离机器人本体设计[J].机器人,2010,32(2):145-149.

[8] 顿向明,闻靖,张育林,等.火箭加注自动对接与脱离机器人有限元分析[J].机械与电子,2011(1):61-64.

备注/Memo

备注/Memo:
收稿日期:2020-09-20
作者简介:黄 钺(1996—),男,江苏南通人,硕士研究生,研究方向为智能机器人;顿向明(1972—),男,安徽宿州人,副教授,硕士研究生导师,研究方向为特种机器人设计、智能机器人。
更新日期/Last Update: 2020-12-28