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Implementation of Sensor-embedded Main Wing Model for Structural Health Monitoring of the Ultra Light Airplane  

Song, Jae-Hoon (항공안전기술개발사업단)
Yang, Jae-Won (단암시스템즈(주))
Rim, Mi-Sun (한국과학기술원 항공우주공학전공)
Kim, Yoon-Young (한국과학기술원 항공우주공학전공)
Park, Hoon (단암시스템즈(주))
Seok, Jong-Nak (단암시스템즈(주))
Kim, Chun-Gon (한국과학기술원 항공우주공학전공)
Choi, Sun-Woo (항공안전기술개발사업단)
Lee, Jang-Yeon (항공안전기술개발사업단)
Publication Information
Aerospace Engineering and Technology / v.11, no.1, 2012 , pp. 178-184 More about this Journal
Abstract
In this study, implementation process of sensor-embedded main wing model for structural health monitoring is described. Fiber Bragg Grating (FBG) Sensor, Plumbum-Zirconate-Titanate (PZT) Sensor, and strain gauge are installed in the main wing of Jabiru UL airplane as a test-bed of Health and Usage Monitoring System (HUMS).
Keywords
Health and Usage Monitoring System; HUMS; Ultra Light Airplane; Fiber Bragg Grating Sensor; Plumbum-Zirconate-Titanate Sensor; Straing Gauge;
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  • Reference
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