流体机械
流體機械
류체궤계
FLUID MACHINERY
2013年
6期
46-49,10
,共5页
压缩机%高压气缸%裂纹失效分析%有限元应力计算
壓縮機%高壓氣缸%裂紋失效分析%有限元應力計算
압축궤%고압기항%렬문실효분석%유한원응력계산
pressure compressor%high-pressure cylinder%broken failure analysis%finite element stress calculation
高压压缩机高压缸阀座底部截面过度处裂纹,通过有限元应力分析,发现压缩机高压气缸阀腔底径厚度不够,阀腔底径偏小,由此对阀腔底径厚度和阀腔底径进行了设计改进,改进后的气缸未再开裂。
高壓壓縮機高壓缸閥座底部截麵過度處裂紋,通過有限元應力分析,髮現壓縮機高壓氣缸閥腔底徑厚度不夠,閥腔底徑偏小,由此對閥腔底徑厚度和閥腔底徑進行瞭設計改進,改進後的氣缸未再開裂。
고압압축궤고압항벌좌저부절면과도처렬문,통과유한원응력분석,발현압축궤고압기항벌강저경후도불구,벌강저경편소,유차대벌강저경후도화벌강저경진행료설계개진,개진후적기항미재개렬。
Abstrast: High-pressure cylinder occurred Cracks ,the Cracks start at the bottom of valve chambers transition section .From fi-nite element stress calculation, the bottom thickness of valve chamber in the high -pressure broken cylinder is not enough , and the passage section of valve chamber is also not enough , so the design of valve chamber is improved ,after improvement,Cracks to high-pressure cylinder have not occurred anymore .