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高空升降框架的结构优化与有限元分析

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沙漠环境中易出现的极端风载对设备的安全性能提出极高要求,现有高空升降框架的设计主要依靠工程经验,存在用料多、自重大、安全余量高等不足.针对此,采用CREO软件建立高空升降框架的三维实体模型,根据国标规定将风载等效为静载荷,采用ANSYS软件对极端风载作用下高空升降框架力学特性进行仿真计算.结果表明:系统与风载不存在共振风险,极限风载作用下系统最大应力幅值为166 MPa.进一步提出设计精细、造价经济的高空升降框架优化设计方案,在极限风载作用下,优化框架静力学计算结果表明:优化后系统的最大应力幅值在降低约35%的同时,可实现整体减重约17%.
Structural Optimization and Finite Element Analysis of High Altitude Lifting Frames
The extreme wind loads that tend to occur in the desert environment place high demands on the safety performance of the equipment,the design of the high altitude lifting frame mainly relies on engineering experience,which has deficiencies in terms of more materials used,higher self-weight and higher safety margin.In view of this,CREO software was used to establish a 3D solid model of high altitude lifting frame,the wind load was equate to static load according to the national standard,and ANSYS software was used to simulate the mechanical characteristics of high altitude lifting frame under extreme wind load.The calculation results show that there is no risk of resonance between the system and the wind load,and the maximum stress amplitude of the system under the extreme wind load is 166 MPa.An optimized design of high altitude lifting frame with fine design and economic cost was further proposed.The results of the statics calculation of the optimized frame under extreme wind load show that the maximum stress amplitude of the optimized sys-tem is reduced by about 35%,while the overall weight reduction of about 17%can be achieved.

high altitude lifting framewind loadstaticsoptimized design

姜展超、丁怀平、高程、张林

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南京理工大学物理学院,江苏南京 210094

江苏开放大学信息工程学院,江苏南京 214257

高空升降框架 风载 静力学 优化设计

国家自然科学基金青年科学基金项目

12002164

2024

机床与液压
中国机械工程学会 广州机械科学研究院有限公司

机床与液压

CSTPCD北大核心
影响因子:0.32
ISSN:1001-3881
年,卷(期):2024.52(12)
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