航天制造技术
航天製造技術
항천제조기술
HANGTIAN ZHIXAO JI SHU
2013年
2期
27-31
,共5页
何凯%邹文兵%李宝辉%肖旅%孙敏杰%李中权
何凱%鄒文兵%李寶輝%肖旅%孫敏傑%李中權
하개%추문병%리보휘%초려%손민걸%리중권
稀土%耐热镁合金%Mg-Gd-Y-Zr 系合金%力学性能%阻尼行为
稀土%耐熱鎂閤金%Mg-Gd-Y-Zr 繫閤金%力學性能%阻尼行為
희토%내열미합금%Mg-Gd-Y-Zr 계합금%역학성능%조니행위
rare earth%heat-resistant magnesium alloy%Mg-Gd-Y-Zr alloy%properties%damping behavior
采用砂型铸造方法,制备了不同Gd含量Mg-Gd-Y-Zr系合金,研究了不同Gd含量对Mg-Gd-Y-Zr系合金室温和高温力学性能、显微组织、阻尼行为的影响.结果表明:当Gd含量达到10%时,室温抗拉强度(T6)达到360MPa,延伸率为4.5%,GW123K合金脆性增加;合金200℃时抗拉强度(T6)仍达到300MPa;低Gd含量的阻尼值高于高Gd含量,GW103K应变振幅ε=0.15×10-2时,Q-1约为0.027.
採用砂型鑄造方法,製備瞭不同Gd含量Mg-Gd-Y-Zr繫閤金,研究瞭不同Gd含量對Mg-Gd-Y-Zr繫閤金室溫和高溫力學性能、顯微組織、阻尼行為的影響.結果錶明:噹Gd含量達到10%時,室溫抗拉彊度(T6)達到360MPa,延伸率為4.5%,GW123K閤金脆性增加;閤金200℃時抗拉彊度(T6)仍達到300MPa;低Gd含量的阻尼值高于高Gd含量,GW103K應變振幅ε=0.15×10-2時,Q-1約為0.027.
채용사형주조방법,제비료불동Gd함량Mg-Gd-Y-Zr계합금,연구료불동Gd함량대Mg-Gd-Y-Zr계합금실온화고온역학성능、현미조직、조니행위적영향.결과표명:당Gd함량체도10%시,실온항랍강도(T6)체도360MPa,연신솔위4.5%,GW123K합금취성증가;합금200℃시항랍강도(T6)잉체도300MPa;저Gd함량적조니치고우고Gd함량,GW103K응변진폭ε=0.15×10-2시,Q-1약위0.027.
In order to improve the heat resistance of the magnesium alloy, the different content of Gd of Mg-Gd-Y-Zr alloy was prerared. And the influence of the different content of Gd to the mechanical properties at room and high temperature and microstructure and damping behavior was researched. The results show that the room temperature tensile strength reached to 360MPa and the elongation reached to 4.5% when Gd content is 10%, but the brittleness of GW123K increased. The high temperature tensile strength still reached to 300MPa at 200℃. Damping properties of the low content is higher than the high content of Gd. When the strain amplitude (ε) of GW103K is 0.15, Q-1 is about 0.027.