中国航空制造技术研究院金属材料技术研究所,北京,100024
纸质出版:2026
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刘莹莹, 王富鑫, 马小昭, 等. TiBw/TA15复合材料持久/蠕变变形行为研究[J]. 航空制造技术, 2026,69(1/2).
LIU Yingying, WANG Fuxin, MA Xiaozhao, et al. Study on Endurance/Creep Deformation Behavior of TiB/TA15 Composite[J]. Aeronautical Manufacturing Technology, 2026, 69(1/2).
刘莹莹, 王富鑫, 马小昭, 等. TiBw/TA15复合材料持久/蠕变变形行为研究[J]. 航空制造技术, 2026,69(1/2). DOI: 10.16080/j.issn1671-833x.20240426.
LIU Yingying, WANG Fuxin, MA Xiaozhao, et al. Study on Endurance/Creep Deformation Behavior of TiB/TA15 Composite[J]. Aeronautical Manufacturing Technology, 2026, 69(1/2). DOI: 10.16080/j.issn1671-833x.20240426.
研究了TiB
w
/TA15 复合材料固溶– 时效热处理过程中的显微组织演变及持久和蠕变变形行为。结果表明,硅化物形态、尺寸和析出位置受热处理时效阶段温度、时间、晶体缺陷及持久/ 蠕变变形过程的影响。较高的时效温度和较长的时效时间及热处理后位错等晶体缺陷的存在是大颗粒硅化物析出、聚集的主要原因。适当提高时效温度可促进α
2
相细小弥散析出,延长时效时间使得α
2
相存在粗化聚集倾向。热处理后持久和蠕变性能受硅化物和α
2
相的共同影响,其中硅化物大量析出和大尺寸硅化物的存在会降低复合材料的持久断裂时间。持久变形过程中位错运动主要发生于α片层内,晶内α
2
相及晶须增强相有效地阻碍了位错运动。持久变形过程中晶须断裂引发的裂纹扩展是造成复合材料持久断裂时间整体偏短的主要原因。在650 ℃ /100 MPa/100 h的测试条件下,TiB
w
/TA15复合材料的蠕变过程受α 晶内、β 晶间位错运动及析出相与位错相互作用的共同影响。
The microstructure evolution and endurance and creep deformation behavior of TiB
w
/TA15 composites during solution–aging heat treatment were studied. The results demonstrate that the silicide morphology
size and precipitation location are affected by temperature
time
crystal defects and endurance and creep deformation process during the heat treatment. High aging temperature
long aging time and the existence of crystal defects such as dislocations after heat treatment are the main causes for the precipitation and aggregation of large-grained silicide. Properly increasing the aging temperature will help to achieve fi
ne dispersion and precipitation of the α
2
phase
and the α
2
phase tends to coarsen and aggregate when the aging time is prolonged. After heat treatment
the endurance and creep properties are affected by the silicide and α
2
phase
among which
the silicide with large amount of precipitation and large size shortens the endurance time of fracture of the composite. The dislocations occurring in the durable deformation process mainly occurs in α layer
which would be impeded by the intragranular α
2
phase and its whiskers. The crack propagation caused by whisker fracture during durable deformation process is the main reason why the general endurance time of fracture of the composite is short. At the testing conditions of 650 ℃ /100 MPa/100 h
the creep process of TiB
w
/TA15 composite is mainly affected by dislocations exiting in intragranular α and β phases and the interactions between precipitations and dislocations.
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