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Defect reduction in (1120) a-plane GaN by two-stage epitaxial lateral overgrowth

机译:两阶段外延横向过生长来减少(1120)a面GaN中的缺陷

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The authors report a two-stage epitaxial lateral overgrowth (ELO) method to get uniformly coalesced (1120) a-plane GaN using metal organic chemical vapor deposition by employing a relatively lower growth temperature in the first stage followed by conditions leading to enhanced lateral growth in the second. Using a two-stage ELO method the average Ga-polar to N-polar wing growth rate ratio has been reduced from 4-6 to 1.5-2, which consequently reduced the height difference between the two approaching wings at the coalescence front that resulted from the wing tilt (0.44° for Ga and 0.37° for N wings, measured by x-ray diffraction), thereby making their coalescence much easier. Transmission electron microscopy showed that the threading dislocation density in the wing areas was 1.0 X 10~8 cm~(-2), more than two orders of magnitude lower than that in the window areas (4.2 X 10~(10) cm~(-2)). However, high density of basal stacking faults of 1.2 X 10~4 cm~(-1) was still present in the wing areas as compared to c-plane GaN where they are rarely observed away from the substrate. Atomic force microscopy and photoluminescence measurements on the coalesced ELO a-plane GaN sample also indicated improved material quality.
机译:作者报告了一种两阶段外延横向过生长(ELO)方法,通过在第一阶段采用相对较低的生长温度以及随后导致横向生长增强的条件,利用金属有机化学气相沉积法获得均匀聚结的(1120)a面GaN。在第二。使用两阶段ELO方法,Ga极与N极的平均机翼生长率比已从4-6降低至1.5-2,从而减小了两个接近机翼在聚结前沿的高度差,这是由于机翼倾斜度(对于Ga机翼为0.44°,对于N机翼为0.37°,通过X射线衍射测量),从而使它们的合并变得更加容易。透射电子显微镜显示,机翼区域的穿线位错密度为1.0 X 10〜8 cm〜(-2),比窗口区域的穿线位错密度(4.2 X 10〜(10)cm〜(-2)低两个数量级。 -2))。然而,与c面GaN相比,在机翼区域仍然存在1.2 X 10〜4 cm〜(-1)的高密度基底堆叠断层,而在c面GaN中,它们很少在远离基板的地方观察到。聚结的ELO a平面GaN样品的原子力显微镜和光致发光测量也表明材料质量得到改善。

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