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可调静叶枢轴泄漏特性的实验研究与结构改进

刘佳欢 孔晓治 陈燕 刘高文

刘佳欢, 孔晓治, 陈燕, 等. 可调静叶枢轴泄漏特性的实验研究与结构改进[J]. 航空动力学报, 2026, 41(8):20250126 doi: 10.13224/j.cnki.jasp.20250126
引用本文: 刘佳欢, 孔晓治, 陈燕, 等. 可调静叶枢轴泄漏特性的实验研究与结构改进[J]. 航空动力学报, 2026, 41(8):20250126 doi: 10.13224/j.cnki.jasp.20250126
Liu Jiahuan, Kong Xiaozhi, Chen Yan, et al. Experimental study and structural improvement of leakage characteristics of variable stator vane pivot[J]. Journal of Aerospace Power, 2026, 41(8):20250126 doi: 10.13224/j.cnki.jasp.20250126
Citation: Liu Jiahuan, Kong Xiaozhi, Chen Yan, et al. Experimental study and structural improvement of leakage characteristics of variable stator vane pivot[J]. Journal of Aerospace Power, 2026, 41(8):20250126 doi: 10.13224/j.cnki.jasp.20250126

可调静叶枢轴泄漏特性的实验研究与结构改进

doi: 10.13224/j.cnki.jasp.20250126
基金项目: 国家自然科学基金(52476025);航空科学基金(2024M070053001)
详细信息
    作者简介:

    刘佳欢(1995-),男,博士生,主要研究方向为航空发动机空气系统封严。E-mail:13759970435@163.com

    通讯作者:

    孔晓治(1989-),男,副教授,博士,主要研究方向为叶轮机械泄漏与主流耦合。E-mail:xzkong@nwpu.edu.cn

  • 中图分类号: V231.1

Experimental study and structural improvement of leakage characteristics of variable stator vane pivot

  • 摘要:

    压气机可调静叶枢轴与机匣之间存在间隙泄漏,对压气机效率有直接影响。为获得枢轴间隙的泄漏特性,搭建了高压比的枢轴泄漏实验平台。通过质量流量控制法和压力损失法,测量不同间隙和进出口压比下的空气泄漏率,分析了枢轴与机匣的配合状态、轴向间隙和径向间隙等对泄漏率的影响。实验结果表明:压比、轴向和径向间隙的增大,会导致泄漏率和质量流量系数的增长;在压比为3.3的工况下,径向接触状态的泄漏率相对于0.01 mm间隙状态降低了86.54%;枢轴的偏心会导致泄漏率增加,而倾斜会导致泄漏率降低。为减少泄漏,对泄漏的流动特性进行仿真分析,并提出了空腔填充简单衬套或篦齿衬套的封严结构。仿真计算结果表明:在压比为3.3的工况下,增加简单衬套后泄漏率下降约为40.04%,增加篦齿衬套后泄漏率下降约为31.8%。

     

  • 图 1  枢轴与机匣装配结构图

    Figure 1.  Pivot and casing assembly structure diagram

    图 2  单衬套与双衬套枢轴结构

    Figure 2.  Single bushing and double bushing pivot structure

    图 3  枢轴同心、倾斜与偏心状态

    Figure 3.  Pivot concentric, tilted and eccentric states

    图 4  实验系统示意图

    Figure 4.  Schematic diagram of the experimental system

    图 5  实验段结构示意图

    Figure 5.  Schematic diagram of the structure of the experimental section

    图 6  部分枢轴实验件

    Figure 6.  Some pivot experimental components

    图 7  基于流量控制法的泄漏率测量过程

    Figure 7.  Leakage rate measurement process based on the flowmeter method

    图 8  基于压力损失的泄漏率测量过程

    Figure 8.  Leakage rate measurement process based on pressure loss

    图 9  两种微小流量测量方法的实验对比

    Figure 9.  Experimental comparison of two microflow measurement methods

    图 10  0#枢轴不同状态下的泄漏率与流量系数

    Figure 10.  0# pivot leakage rate and flow coefficient in different states

    图 11  4#枢轴不同状态下的泄漏率与流量系数

    Figure 11.  4# pivot leakage rate and flow coefficient in different states

    图 12  使用压力损失法测量枢轴接触泄漏率

    Figure 12.  Pivot contact leakage rate measured by the transient pressure method

    图 13  4#枢轴不同径向间隙下的泄漏率与流量系数

    Figure 13.  4# pivot leakage rate and flow coefficient under different radial clearances

    图 14  0#枢轴不同姿态下的泄漏率与流量系数

    Figure 14.  0# pivot leakage rate and flow coefficient under different attitudes

    图 15  不同枢轴长度下的泄漏率与流量系数

    Figure 15.  Leakage rate and flow coefficient at different pivot lengths

    图 16  枢轴泄漏流动区域及网格划分

    Figure 16.  Pivot leakage flow area and meshing

    图 17  压比为2.5工况下的原始结构速度云图

    Figure 17.  Velocity contour diagram of the original structure at pressure ratio of 2.5

    图 18  压比为2.5工况下的原始结构压力云图

    Figure 18.  Pressure contour diagram of the original structure at pressure ratio of 2.5

    图 19  完全偏心状态实验数据与仿真计算对比图

    Figure 19.  Comparison of experimental data and simulation calculations in complete eccentric state

    图 20  两种改进密封结构示意图

    Figure 20.  Schematic diagram of two improved seal structures

    图 21  压比为2.5工况下的改进结构1速度云图

    Figure 21.  Velocity contour diagram of the improved structure 1 at pressure ratio of 2.5

    图 22  压比为2.5工况下的改进结构1压力云图

    Figure 22.  Pressure contour diagram of the improved structure 1 at pressure ratio of 2.5

    图 23  压比为2.5工况下的改进结构2速度云图

    Figure 23.  Velocity contour diagram of the improved structure 2 at pressure ratio of 2.5

    图 24  压比为2.5工况下的改进结构2压力云图

    Figure 24.  Pressure contour diagram of the improved structure 2 at pressure ratio of 2.5

    图 25  原始结构与改进结构泄漏率对比

    Figure 25.  Comparison of leakage rates between the original structure and the improved structures

    图 26  原始结构的空腔流动

    Figure 26.  Cavity flow of the original structure

    图 27  改进结构2的空腔流动

    Figure 27.  Cavity flow of improved structure 2

    表  1  实验件间隙组别设置

    Table  1.   Setup of the gap categories for the experimental components

    编号 枢轴结构 枢轴长度
    $ L $/mm
    轴向间隙
    $ a $/mm
    径向间隙
    $ c $/mm
    0# 单衬套 19.5 0.06 0.2
    0.11
    0.17
    1# 双衬套 29.9 0.07 0.2
    0.12
    0.18
    2# 双衬套 27.5 0.09 0.2
    0.12
    0.18
    3# 双衬套 32.7 0.07 0.2
    0.12
    0.18
    4# 双衬套 48.3 0.08 0~0.3
    0.09
    0.12
    下载: 导出CSV

    表  2  主要参数的不确定度

    Table  2.   Uncertainty of the main parameters

    参数不确定度/%
    $ \Delta A/A $1.5
    $ \Delta \dot{m}/\dot{m} $1
    $ \Delta {\dot{m}}_{\text{id}}/{\dot{m}}_{\text{id}} $1.53
    $ \Delta {C}_{\text{d}}/{C}_{\text{d}} $1.83
    下载: 导出CSV
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  • 收稿日期:  2025-03-13
  • 网络出版日期:  2026-06-01

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