Title :
Implementation of sensor-embedded main wing model of ultra light airplane for health and usage monitoring system (HUMS) test-bed
Author :
Song, Jae-Hoon ; Yang, Jae-Won ; Rim, Mi-Sun ; Kim, Yoon-Young ; Kim, Ji-Hwan ; Park, Hoon ; Seok, Jong-Nak ; Kim, Chun-Gon ; Lee, Hyeong-Chul ; Choi, Sun-Woo ; Lee, Jang-Yeon
Author_Institution :
Aviation Safety R&D Center, Korea Aerosp. Res. Inst., Daejeon, South Korea
Abstract :
In this paper, development process of sensor-embedded main wing model as a test-bed of HUMS is described. Fiber Bragg Grating (FBG) Sensor, Plumbum-Zirconate-Titanate (PZT) Sensor, Acceleration Sensor, and Strain gauge are installed in the main wing. These sensors are located on the surface of the spar, the upper skin and the aileron of an ultra light airplane as a target aircraft. Each sensor is tested for operation status during the installation process.
Keywords :
Bragg gratings; acceleration; aerospace accidents; aerospace components; aircraft; condition monitoring; optical fibres; sensor placement; strain gauges; FBG sensor; HUMS test-bed; PZT sensor; acceleration sensor; aileron; fiber Bragg grating sensor testing; health-and-usage monitoring system test-bed; installation process; operation status; plumbum-zirconate-titanate sensor; sensor-embedded main wing model; spar surface; strain gauge; target aircraft; ultra-light airplane; upper skin; Aircraft; Aircraft manufacture; Fiber gratings; Monitoring; Safety; Skin; Acceleration Sensor; Fiber Bragg Grating (FBG) Sensor; Health and Usage Monitoring System (HUMS); Plumbum-Zirconate-Titanate (PZT) Sensor; Strain Gauge; Ultra Light Airplane;
Conference_Titel :
Control, Automation and Systems (ICCAS), 2012 12th International Conference on
Conference_Location :
JeJu Island
Print_ISBN :
978-1-4673-2247-8
