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초소성 및 확산접합을 이용한 우주항공 부품 성형기술 개발
이호성,윤종훈,이영무,Lee, Ho-Sung,Yoon, Jong-Hoon,Yi, Yeong-Moo 한국군사과학기술학회 2005 한국군사과학기술학회지 Vol.8 No.3
In this paper, a near net shape technology using superplasticity and diffusion bonding characteristics was presented for application to various components of aircraft and missiles. Due to these special characteristics of some aerospace alloys, it is possible to produce complex components to shape very near final dimension with enhanced design freedom, reduced material usage, and overall saving of weight and cost. The high pressure vessel for a space launcher was fabricated with Ti-6Al-4V alloy by superplastic forming and diffusion bonding process and the failure characteristics are compared with conventionally fabricated vessel spin formed and TIG welded. The structural integrity of the superplastic forming and diffusion bonding process was successfully demonstrated.
Ti-6Al-4V 샌드위치 패널제작을 위한 초소성/확산접합 기술개발
이호성,윤종훈,이승철,박동규,이영무,Lee, Ho-Sung,Yoon, Jong-Hoon,Lee, Seung-Chul,Park, Dong-Kyu,Yi, Yeong-Moo 한국군사과학기술학회 2008 한국군사과학기술학회지 Vol.11 No.3
Ti-6Al-4V alloy is a critical strategic metal used in aerospace structure due to the high specific strength, toughness, durability, low density, corrosion resistance. Examples of application of this alloy are airframe structural components, aircraft gas turbine disks and blades. Forming of this alloy is not easy due to its high strength and low formability. However, this alloy shows superplastic properties that allow for large plastic deformation under certain conditions. Combination of superplastic forming and diffusion bonding(SPF/DB) processes of this alloy has been widely used to replace mechanically fastened structures with reduced weight and fabrication costs. In this study, superplastic forming/diffusion bonding technology has been developed for fabricating lightweight sandwich panels with Ti-6Al-4V alloy. The experimental results show the forming of titanium lightweight sandwich structure is successfully performed from 3 and 4 sheets of Ti-6Al-4V.
공철원(Cheol-Won Kong),남기원(Gi-Won Nam),이영무(Yeong-Moo Yi),Akira Ohnishi 한국항공우주연구원 2011 항공우주기술 Vol.10 No.1
다공성 소재의 열 확산도 측정 시스템을 개발하였다. 열확산도를 측정하는 다양한 시스템이 있지만 다공성 소재의 열확산도를 측정하는 것은 기존의 시스템으로는 어렵다. 본 논문에서는 주기가열법을 이용한 열확산도 측정시스템 및 장비의 검증에 대하여 정리하였다. 주기가열법을 검증하기 위해서 사용한 표준시편은 세라믹 소재를 사용하였다. 그 결과 표준값과 측정값이 일치함을 보였다. 다공성 소재 적용을 위하여 검증한 시편은 폴리스티렌폼이었다. 진공에서 열확산도 값도 측정하였는데, 진공에서 열확산도는 대기조건과 비교하여 63% 감소함을 보였다. 두 결과 모두 측정값과 표준값은 10% 오차 범위 이내에 있었다. A system of measurement for the thermal diffusivity of porous materials was developed. Although there are several measurement systems for thermal diffusivity, it is typically difficult to measure the thermal diffusivity of porous materials. This paper presents a measurement system for thermal diffusivity that utilizes a cyclic heating method along with the verification of the measured device. To verify the cyclic heating method, the available reference data of aceramic specimen was utilized. To apply the system to an actual porous material, polystyrene foam was tested. The thermal diffusivity of the polystyrene foam under vacuum was reduced by 63%. The measured values from both tests were in good agreement with the reference values, as they were within 10% of these values.