首页|新型变壁厚涡旋型线的构建与性能研究

新型变壁厚涡旋型线的构建与性能研究

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为解决等壁厚涡旋型线压缩比低、结构不紧凑、传统变壁厚涡旋型线气体力变化幅度大的问题,设计了一种由基圆渐开线、高次曲线和变基圆渐开线组合的新型变壁厚涡旋型线,并建立了该型线的基本几何理论.为定量衡量该型线的性能,特引入表征型线几何性能的两个关键指标—压缩比和体积利用系数以及力学性能的两个重要指标—轴向气体力和切向气体力对其进行评价.研究结果表明:新型变壁厚型线的几何性能与力学性能受半径变换率的影响较大,在相同设计条件下,随着半径变换率的减小,不仅压缩比和体积利用系数显著提高,而且所承受的轴向气体力和切向气体力的变化幅度也明显变小.可见,采用半径变换率较小的新型变壁厚型线有助于进一步提升涡旋型线的性能.
Construction and Performances Research on a New Type of Variable Wall Thickness Scroll Profile
To solve the problems of low compression ratio and uncompacted structure of scroll profile with equal wall thickness,and the large variation range of gas force of traditional variable wall thickness scroll profile,a new type of scroll profile with variable wall thickness was designed,which was composed of base circle involute,high-order curve and variable base circle involute,and the basic geometric theory of the profile was established.In order to quantitatively measure the performance of the scroll profile,two key indicators representing the geometric performance of the profile,which is compression ratio and volume utilization coefficient,and two important indicators of mechanical performance,namely axial and tangential gas force were introduced to evaluate the profile.The research results show that the geometric and mechanical performances of the new variable wall thickness scroll profile are greatly affected by the radius transformation rate.Under the same design conditions,with the decrease of the radius transformation rate,not only the compression ratio and the volume utilization coefficient are significantly improved,but also the variation range of the axial and tangential gas forces are significantly reduced.It can be seen that the adoption of a new type of variable wall thickness profile with smaller radius transformation rate will help further improve the performance of the scroll profile.

scroll compressorvariable wall thickness profilegeometric performancemechanical performanceradius transformation rate

侯才生、刘宇、李金虎

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宁夏大学机械工程学院,宁夏 银川 750021

涡旋压缩机 变壁厚型线 几何性能 力学性能 半径变换率

宁夏自然科学基金

2022AAC03101

2024

压缩机技术
沈阳气体压缩机研究所

压缩机技术

影响因子:0.303
ISSN:1006-2971
年,卷(期):2024.(1)
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