This paper presents ESPI system for the measurement of thermal expansion coefficient of STS430 up to 1,000℃ Existing methods, strain gauge and moire have the limitation of contact to object and do not supply the coefficient up to 800℃ There need...
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https://www.riss.kr/link?id=A76214616
2004
Korean
550
학술저널
20-24(5쪽)
0
상세조회0
다운로드다국어 초록 (Multilingual Abstract)
This paper presents ESPI system for the measurement of thermal expansion coefficient of STS430 up to 1,000℃ Existing methods, strain gauge and moire have the limitation of contact to object and do not supply the coefficient up to 800℃ There need...
This paper presents ESPI system for the measurement of thermal expansion coefficient of STS430 up to 1,000℃ Existing methods, strain gauge and moire have the limitation of contact to object and do not supply the coefficient up to 800℃ There needs to measure the data up to 800℃ because heat resistant materials have high melting temperature up to 1,000℃ In previous studies related to thermal strain analysis, the quantitative results are not reported by ESPI at high temperature, yet. In-plane ESPI and vacuum chamber for the reduction of air turbulence and oxidation are designed for the measurement of the coefficient up to 1,000℃ and speckle correlation fringe pattern images are processed by commercial image filtering tool-smoothing, thinning and enhancement- to obtain quantitative results, which is compared with references data. The comparison shows two data are agreed within 4.1% blow 600℃ however, there is some difference up to 600℃ Also, the incremental ratio of the coefficient is changed up to 800℃ The reason is the phase transformation of STS430 probably begins at 800℃.
목차 (Table of Contents)
항공기 기체 부품 생산을 위한 생산 현장 중심의 설계 생산 통합 / 정보 시스템 개발
5-Head Router Machine 의 이면 구속 공구 시스템
기업 정보 시스템간 효율적인 데이터 공유를 위한 통합 도구 개발