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复杂薄壁壳体流固耦合仿真分析及试验研究

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针对某涡轮增压器复杂薄壁燃进壳漏水现象,采用 CFD 流固耦合计算方法,分别仿真模拟了柴油机运行工况及增压器试验台运行工况温度、应力分布,并开展了试验测试.研究表明:燃进壳温度场分布均匀无突变,柴油机工况下燃进壳表面最高温度为 212℃,最低温度为 72℃,台位试验工况下,燃进壳表面最高温度为 193.6℃,比柴油机工况减小 18.4℃,台位试验测试与仿真模拟高度吻合,最大误差约为 4.3%.应力计算表明:燃进壳应力分布均匀,柴油机工况下,最大等效应力为 176 MPa,最大等效应力小于材料屈服强度 224MPa,安全系数 1.27,台位试验工况下,最大等效应力分布在燃进壳冷却水流道,最大值约为 230 MPa.燃进壳理论计算应变与实际测试应变最大误差为 4.11%,理论计算结果与实际测试结果吻合较好,燃进壳应力计算完全满足工程仿真精度要求,研究结成果为后续燃进壳寿命提升奠定理论计算基础.
Simulation Analysis of Fluid-structure Coupling Strength of Complex Thin-walled Shells and Experimental Testing
Based on the finite element method,For a turbocharger complex thin-walled combustion inlet shell leakage phenomenon,Using CFD fluid-solid coupling calculation method,The temperature and stress distribu-tion of the diesel engine and turbocharger test rig were simulated respectively,and experiments were conducted.The study shows that the combustion inlet shell temperature field is uniformly distributed without abrupt chan-ges,The maximum temperature of the surface of the combustion inlet shell under diesel engine operating condi-tions is 212℃,and the minimum temperature is 72℃.Under the bench test condition,the maximum tempera-ture of the surface of the combustion shell is 193.6℃,which is 18.4℃less than that of the diesel engine,and the minimum temperature of the inner cavity is 20℃.The bench test is in high agreement with the simulation,with a maximum error of about 4.3%.Stress calculations show that:combustion into the shell stress is equally distributed,diesel engine conditions,the maximum equivalent force of 176 MPa,the maximum equivalent force is less than the yield strength of the material 224MPa,the safety factor of 1.27.Under the bench test condition,the maximum stress was distributed in the combustion inlet shell cooling water flow path,with a maximum value of about 230 MPa.The maximum error between the theoretical calculated strain and the actual test strain of the combus-tion shell is 4.11%,the theoretical calculation results and the actual test results are in good agreement,and the stress calculation of the combustion shell fully meets the requirements of the engineering simulation accuracy,and the results of the study lay the theoretical calculation basis for the subsequent enhancement of the combustion shell life.

TurbochargerGas intake housingFluid-solid couplingTemperatureStresses

吴旭辉、王文鼎、黄礼洋、唐国庆

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海装广州局驻重庆地区第二军事代表室,重庆 400042

重庆江增船舶重工有限公司,重庆 402284

涡轮增压器 燃进壳 流固耦合 温度 应力

2024

内燃机与配件
石家庄金刚内燃机零部件集团有限公司

内燃机与配件

影响因子:0.095
ISSN:1674-957X
年,卷(期):2024.(7)
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