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[InAs/GaSb] 응력 초격자에 기초한 [320×256]-FPA 적외선 열영상 모듈 제작
이상준,노삼규,배수호,정한,Lee, S.J.,Noh, S.K.,Bae, S.H.,Jung, H. 한국진공학회 2011 Applied Science and Convergence Technology Vol.20 No.1
An infrared thermographic imaging module of [$320{\times}256$] focal-plane array (FPA) based on [InAs/GaSb] strained-layer superlattice (SLS) was fabricated, and its images were demonstrated. The p-i-n device consisted of an active layer (i) of 300-period [13/7]-ML [InAs/GaSb]-SLS and a pair of p/n-electrodes of (60/115)-period [InAs:(Be/Si)/GaSb]-SLS. FTIR photoresponse spectra taken from a test device revealed that the peak wavelength (${\lambda}_p$) and the cutoff wavelength (${\lambda}_{co}$) were approximately $3.1/2.7{\mu}m$ and $3.8{\mu}m$, respectively, and it was confirmed that the device was operated up to a temperature of 180 K. The $30/24-{\mu}m$ design rule was applied to single pixel pitch/mesa, and a standard photolithography was introduced for [$320{\times}256$]-FPA fabrication. An FPA-ROIC thermographic module was accomplished by using a $18/10-{\mu}m$ In-bump/UBM process and a flip-chip bonding technique, and the thermographic image was demonstrated by utilizing a mid-infrared camera and an image processor. InAs/GaSb 제2형 응력초격자(SLS)를 활성층에 탑재한 [$320{\times}256$] 초점면 배열(FPA) 적외선 열영상 모듈을 제작하고 열영상을 구현하였다. p-i-n형으로 설계된 소자의 활성층(i) 구조는 300 주기의 [13/7]-ML [InAs/GaSb]-SLS로 구성되어 있고, p와 n 전극층에는 각각 60주기의 [InAs:Be/GaSb]-SLS와 115 주기의 [InAs:Si/GaSb]-SLS 구조를 채용하였다. 시험소자의 광반응(PR) 스펙트럼으로부터 피크 파장(${\lambda}_p$)과 차단 파장(${\lambda}_{co}$)은 각각 ${\sim}3.1/2.7{\mu}m$과 ${\sim}3.8{\mu}m$이고 180 K 온도까지 동작을 확인하였다. 단위 화소의 간격/메사는 $30/24{\mu}m$ 규격으로 설계되었으며, [$320{\times}256$]-FPA는 표준 광묘화법으로 제작하였다. $18/10{\mu}m$의 In-bump/UBM 공정과 flip-chip 결합 기술을 적용하여 FPA-ROIC 열영상 모듈을 완성하였으며, 중적외선용 영상구동 회로 및 S/W를 활용하여 열영상을 시연하였다.
직접분사식 가솔린 선회 분사기에서의 내부 유동특성에 관한 수치 해석
배수호(S . H . Bae),문수연(S . Y . Moon),이충원(C . W . Lee) 한국분무공학회 2001 한국액체미립화학회지 Vol.6 No.2
The internal flow characteristics of a gasoline direct injector have been studied to improve fuel economy and reduce exhaust emissions. Computational Fluid Dynamics (CFD) is used to examine the internal flow of the GDI with the purpose of designing the optimum geometry of the injector. This study tests orifice length, cone angle, swirl angle, orifice diameter and needle lift. The results show that optimum sizes of the orifice length, cone angle, swirl angle, orifice diameter and needle lift are 0.8mm, 140mm, 120mm, 80mm and 70mm, respectively. The size of the lift does not affect the formation of the air core significantly near the tip of the needle compared to the ball-type needle. The vena contracts phenomenon near the orifice inlet can be released by smoothing the edge.