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立式捏合机桨叶型面设计与优化

詹小斌 李锡文 张嘉琪 崔峰

固体火箭技术Issue(3):413-417,5.
固体火箭技术Issue(3):413-417,5.DOI:10.7673/j.issn.1006-2793.2014.00.024

立式捏合机桨叶型面设计与优化

Design and optimization on blade profile of vertical kneader

詹小斌 1李锡文 1张嘉琪 1崔峰2

作者信息

  • 1. 华中科技大学 机械科学与工程学院,武汉 430074
  • 2. 湖北三江航天江河化工科技有限公司,宜昌 444200
  • 折叠

摘要

Abstract

In accordance with the weaknesses of the existing vertical kneaders'blades,based on the vertical kneader's kneading principles and movement characteristics,the existing hollow blades'modeling process was analyzed and evaluated,and new modeling method was proposed.Simulation analysis shows that the hollow blade's kneading range increases by approximately 31.5%.Take the solid blade's non-kneading surface was an example,on the basis of the mechanical properties of the blade,movement characteristics, and processing requirements,the modeling region of non-kneading surface was designed.The contour of the non-kneading surface is redesigned and treated by several circular arcs as well.Under the circumstance that the blade stiffness will not be weakened,simula-tion analysis shows the blade's maximum stress reduces by about 20%. By using the fresh design into practical blade design proce-dure,the mixing performance and mechanical property of the blade are greatly improved.

关键词

立式捏合机/桨叶/捏合面/优化

Key words

vertical kneader/blade/kneading surface/optimization

分类

化学化工

引用本文复制引用

詹小斌,李锡文,张嘉琪,崔峰..立式捏合机桨叶型面设计与优化[J].固体火箭技术,2014,(3):413-417,5.

基金项目

国家重大科学仪器设备开发专项(2011YQ160002);中央高校基本业务费资助(2010MS090)。 ()

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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