采用有限元模态算法和应变模态测量试验对比金属桨和碳纤维桨模型的固有频率、位移和应变模态振型,试验测得铜桨和碳纤维桨的前三阶固有频率与计算值相差分别在3%和12%以内。碳纤维桨各阶固有频率均比铜桨要小,应变模态振型相似,前者结...采用有限元模态算法和应变模态测量试验对比金属桨和碳纤维桨模型的固有频率、位移和应变模态振型,试验测得铜桨和碳纤维桨的前三阶固有频率与计算值相差分别在3%和12%以内。碳纤维桨各阶固有频率均比铜桨要小,应变模态振型相似,前者结构阻尼是后者的4倍左右。计算二者在流域中的湿模态,铜桨的前四阶湿模态固有频率比干模态减小18%~33%,碳纤维桨减小54%~64%。研究铜桨和不同铺层碳纤维桨之间的振动特性,得出有利于减轻振动的纤维铺层方式,优选出的碳纤维桨总振动加速度级（TAL）比试验用碳纤维桨降低2 d B。展开更多
In view of the high cost caused by the 1:1 lifetime verification test of ion thrusters,the lifetime acceleration test should be considered.This work uses the PIC-MCC(Particle-in-Cell MonteCarlo Collision)method to ana...In view of the high cost caused by the 1:1 lifetime verification test of ion thrusters,the lifetime acceleration test should be considered.This work uses the PIC-MCC(Particle-in-Cell MonteCarlo Collision)method to analyze the five failure factors that lead to the failure of the accelerator grid of a 30 cm diameter ion thruster under the working mode of 5 k W.Meanwhile,the acceleration stress levels corresponding to different failure factors are obtained.The results show that background pressure has the highest stress level on the grid's erosion.The accelerator grid aperture's mass sputtering rate under the rated vacuum degree(1×10^(-4)Pa)of 5 k W work mode is 8.78 times that of the baseline vacuum degree(1×10^(-6)Pa),and the mass sputtering rate under worse vacuum degree(5×10^(-3)Pa)is 5.08 times that of 1×10^(-4)Pa.Under the influence of the other four failure factors,namely,the voltage of the accelerator grid,upstream plasma density,the screen grid voltage and mass utilization efficiency,the mass sputtering rates of the accelerator grid hole are 2.32,2.67,1.98 and 2.51 times those of the accelerator grid hole under baseline condition,respectively.The ion sputtering results of two 30 cm diameter ion thrusters(both installed with new grids assembly)after working for 1000 h show that the mass sputtering rate of the accelerator grid hole under vacuum conditions of 5×10^(-3)Pa is 4.54 times that under the condition of 1×10^(-4)Pa,and the comparison error between simulation results and test results of acceleration stress is about 10%.In the subsequent ion thruster lifetime verification,the working vacuum degree can be adjusted according to the acceleration stress level of background pressure,so as to shorten the test time and reduce the test cost.展开更多
文摘采用有限元模态算法和应变模态测量试验对比金属桨和碳纤维桨模型的固有频率、位移和应变模态振型,试验测得铜桨和碳纤维桨的前三阶固有频率与计算值相差分别在3%和12%以内。碳纤维桨各阶固有频率均比铜桨要小,应变模态振型相似,前者结构阻尼是后者的4倍左右。计算二者在流域中的湿模态,铜桨的前四阶湿模态固有频率比干模态减小18%~33%,碳纤维桨减小54%~64%。研究铜桨和不同铺层碳纤维桨之间的振动特性,得出有利于减轻振动的纤维铺层方式,优选出的碳纤维桨总振动加速度级（TAL）比试验用碳纤维桨降低2 d B。
基金supported by Key Laboratory Funds for the Science and Technology on Vacuum Technology and Physics Laboratory,Lanzhou Institute of Physics(Nos.HTKJ2022KL510003 and 6142207210303)Independent project of Hangzhou Institute for Advanced Study(No.2022ZZ01009)Science and Technology Project Affiliated to the Education Department of Chongqing Municipality(No.KJZD-K202101506)。
文摘In view of the high cost caused by the 1:1 lifetime verification test of ion thrusters,the lifetime acceleration test should be considered.This work uses the PIC-MCC(Particle-in-Cell MonteCarlo Collision)method to analyze the five failure factors that lead to the failure of the accelerator grid of a 30 cm diameter ion thruster under the working mode of 5 k W.Meanwhile,the acceleration stress levels corresponding to different failure factors are obtained.The results show that background pressure has the highest stress level on the grid's erosion.The accelerator grid aperture's mass sputtering rate under the rated vacuum degree(1×10^(-4)Pa)of 5 k W work mode is 8.78 times that of the baseline vacuum degree(1×10^(-6)Pa),and the mass sputtering rate under worse vacuum degree(5×10^(-3)Pa)is 5.08 times that of 1×10^(-4)Pa.Under the influence of the other four failure factors,namely,the voltage of the accelerator grid,upstream plasma density,the screen grid voltage and mass utilization efficiency,the mass sputtering rates of the accelerator grid hole are 2.32,2.67,1.98 and 2.51 times those of the accelerator grid hole under baseline condition,respectively.The ion sputtering results of two 30 cm diameter ion thrusters(both installed with new grids assembly)after working for 1000 h show that the mass sputtering rate of the accelerator grid hole under vacuum conditions of 5×10^(-3)Pa is 4.54 times that under the condition of 1×10^(-4)Pa,and the comparison error between simulation results and test results of acceleration stress is about 10%.In the subsequent ion thruster lifetime verification,the working vacuum degree can be adjusted according to the acceleration stress level of background pressure,so as to shorten the test time and reduce the test cost.
