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台阶式斜篦齿封严压降与风阻温升数值分析

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为研究转速、进口压力及齿隙和齿宽的比对斜篦封严压降与风阻温升特性的影响,建立二维阶梯式斜篦齿封严模型,对台梯式斜篦齿封严进行数值仿真计算,获得不同转速、进口压力及齿隙和齿宽的比下的进出口压差和风阻温升,以及最后一级齿隙处射流的温度和压力.结果表明:斜篦齿的背风面存在高温带,主要是由于旋转的摩擦效应、阶梯几何结构和2个大尺寸涡相遇处的掺混效应所导致;贴壁大尺寸涡与主流的动量交换随着转速的增加而增强,主流与齿腔大尺寸涡的动量交换随着转速的增加而减弱;风阻温升随着齿隙和齿宽的比的增大而降低,随着转速的增加而升高,但与进口压力的关系不明显;进出口压差随着转速的增加而增大,随着齿隙和齿宽的比的增大而减小;出口射流的压力随着进口压力的增加而增加.分别得到压差比和风阻温升系数的拟合式,拟合效果符合预期.
Numerical Analysis on Pressure Drop and Wind Resistance Temperature Rise of Stepped Inclined Grate Teeth Sealing
To study the effects of rotational speed,inlet pressure,and the ratio of backlash to tooth width on the pres-sure drop and wind resistance temperature rise characteristics of inclined grate teeth seals,a two-dimensional stepped in-clined grate seal model was established.Numerical simulation calculations were performed on the stepped inclined grate teeth seals to obtain the inlet and outlet pressure differences and wind resistance temperature rise under different speed,inlet pressure,and the ratio of backlash to tooth width,as well as the temperature and pressure of the jet at the last stage tooth gap.It is found that there is a high-temperature zone on the leeward side of the oblique grate tooth,which is caused by three factors,the friction effect of rotation,the step geometry and the mixing effect at the meeting point of two large-size vortices.The momentum exchange between the wall-attached large-size vortex and the main flow increases with the in-crease of rotational speed,while the momentum exchange between the main flow and the large-size vortex in the cavity weakens with the increase of rotational speed.The wind resistance temperature rise decreases with the increase of the ratio of backlash to tooth width,and increases with the increase of rotational speed,but the relationship with the inlet pressure is not obvious.The pressure difference between the inlet and outlet increases with the increase of rotational speed,and de-creases with the increase of the ratio of backlash to tooth width.The pressure of the exit jet increases with the increase of the inlet pressure.The fitting formulas of pressure difference and wind resistance temperature rise coefficient were obtained respectively,and the fitting result was in line with expectations.

sealwind resistance temperature risepressuredata fitting

李驰、张勃、马壮、张靖周、王家友

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南京航空航天大学能源与动力学院,江苏南京 210016

沈阳航空发动机研究所,辽宁沈阳 110000

封严 风阻温升 压力 数据拟合

国家两机重大专项

2017-Ⅲ-0011-0037

2024

润滑与密封
中国机械工程学会 广州机械科学研究院有限公司

润滑与密封

CSTPCD北大核心
影响因子:0.478
ISSN:0254-0150
年,卷(期):2024.49(6)
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