ROTOR PROFILES DESIGN METHOD AND NUMERICAL SIMULATION FOR TWIN-SCREW COMPRESSOR

The rotor profiles are the key factor of twin-screw compressor,but there is some inconvenience in modification and experiment of rotor profile. NURBS curves and computational fluid simulation analysis are applied to overcome these two problems. NURBS curves are introduced to construct a new rotor pr...

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Main Authors: 何雪明, 潘成龙, 武美萍, 纪小刚, 张荣
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2016-01-01
Series:Jixie qiangdu
Subjects:
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2016.02.015
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author 何雪明
潘成龙
武美萍
纪小刚
张荣
author_facet 何雪明
潘成龙
武美萍
纪小刚
张荣
author_sort 何雪明
collection DOAJ
description The rotor profiles are the key factor of twin-screw compressor,but there is some inconvenience in modification and experiment of rotor profile. NURBS curves and computational fluid simulation analysis are applied to overcome these two problems. NURBS curves are introduced to construct a new rotor profile based on the rotor profile of unilateral asymmetric combined cycloid with pin gear arc. The equations of profile are given. The numerical simulation models of the new profile and the original profile are built to find out the distribution law of pressure and velocity in twin-screw compressors under the operating speed by the means of FLUENT software. Finally,according to the simulation results,the rationality of the designed rotor profile is verified,and new schemes for further optimization are explored. Then an experiment is made to describe the reliability and convenience of this design method.
format Article
id doaj-art-a952cab8004b484e828a631db1db8347
institution Kabale University
issn 1001-9669
language zho
publishDate 2016-01-01
publisher Editorial Office of Journal of Mechanical Strength
record_format Article
series Jixie qiangdu
spelling doaj-art-a952cab8004b484e828a631db1db83472025-01-15T02:37:02ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692016-01-013828829430594706ROTOR PROFILES DESIGN METHOD AND NUMERICAL SIMULATION FOR TWIN-SCREW COMPRESSOR何雪明潘成龙武美萍纪小刚张荣The rotor profiles are the key factor of twin-screw compressor,but there is some inconvenience in modification and experiment of rotor profile. NURBS curves and computational fluid simulation analysis are applied to overcome these two problems. NURBS curves are introduced to construct a new rotor profile based on the rotor profile of unilateral asymmetric combined cycloid with pin gear arc. The equations of profile are given. The numerical simulation models of the new profile and the original profile are built to find out the distribution law of pressure and velocity in twin-screw compressors under the operating speed by the means of FLUENT software. Finally,according to the simulation results,the rationality of the designed rotor profile is verified,and new schemes for further optimization are explored. Then an experiment is made to describe the reliability and convenience of this design method.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2016.02.015NURBS curveFluid simulation analysisTwin screw compressorRotor profile
spellingShingle 何雪明
潘成龙
武美萍
纪小刚
张荣
ROTOR PROFILES DESIGN METHOD AND NUMERICAL SIMULATION FOR TWIN-SCREW COMPRESSOR
Jixie qiangdu
NURBS curve
Fluid simulation analysis
Twin screw compressor
Rotor profile
title ROTOR PROFILES DESIGN METHOD AND NUMERICAL SIMULATION FOR TWIN-SCREW COMPRESSOR
title_full ROTOR PROFILES DESIGN METHOD AND NUMERICAL SIMULATION FOR TWIN-SCREW COMPRESSOR
title_fullStr ROTOR PROFILES DESIGN METHOD AND NUMERICAL SIMULATION FOR TWIN-SCREW COMPRESSOR
title_full_unstemmed ROTOR PROFILES DESIGN METHOD AND NUMERICAL SIMULATION FOR TWIN-SCREW COMPRESSOR
title_short ROTOR PROFILES DESIGN METHOD AND NUMERICAL SIMULATION FOR TWIN-SCREW COMPRESSOR
title_sort rotor profiles design method and numerical simulation for twin screw compressor
topic NURBS curve
Fluid simulation analysis
Twin screw compressor
Rotor profile
url http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2016.02.015
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