A solution model of the rotor dynamic characteristics for taper clearance hole-pattern damper seal using unsteady transient solution combined with mesh deformation technique was established. The influences of taper degrees and whirling frequencies on the leakage rates
rotor dynamic characteristics
and suppression vibration mechanism of taper hole-pattern damper seal were studied. Results showed that
the leakage straight-through effect of the hole-pattern damper seals was enhanced by taper clearance
which increased the leakage rates. The leakage rates of convergent-clearance hole-pattern damper seals were less than the divergent-clearance hole-pattern damper seals when there was the same average seal clearance. The stiffness coefficients increased with the increase of taper degrees
while there was an opposite trend for the damping coefficients under the same whirling frequency of the rotor. The convergent-taper hole-pattern damper seals had large posi tive direct stiffness
and increased the natural frequency of rotor system
while divergent-taper hole-pattern damping seals had large negative direct stiffness. The convergent-taper hole-pattern damping seals had large effective stiffness and cross-over frequency
and small effective damping. The divergent-taper hole-pattern damper seals had large effective damping
small efective stiffness and cross-over frequency. The concentricity and the natural frequency of rotor system should be considered when design of taper clearance hole-pattern damper seals.
Mechanism of influence of notch jet⁃flow on leakage and rotordynamic characteristics of pocket damper seals
Mechanism of influence of pre⁃swirl on leakage and rotordynamic characteristics of swirl brake seal
Numerical study on leakage and dynamic characteristics of circumferentially divergent pocket damping seal
基于三维接触摩擦单元的套齿连接解析建模研究
与发动机匹配的旁路式双喉道气动矢量喷管数值模拟研究
Related Author
Yong HU
Jigang MENG
Zhonghui XIAO
Huan ZHAO
Dan SUN
Jindao GUO
Min ZHOU
Guochen ZHANG
Related Institution
Key Laboratory of Advanced Measurement and Test Technology for Aviation Propulsion System,Liaoning Province,School of Aero⁃engine,Shenyang Aerospace University
Collaborative Innovation Center of Machine Manufacturing in Liaoning,Shenyang Blower Works Group Company Limited
Key Laboratory of Advanced Measurement and Test Technology for;Aviation Propulsion System,Liaoning Province,School of Aero⁃engine,Shenyang Aerospace University
Key Laboratory of Advanced Measurement and Test Technique for Aviation Propulsion System,Liaoning Province,School of Aero⁃engine,Shenyang Aerospace University