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

fYear

2012

fDate

17-21 Oct. 2012

Firstpage

1247

Lastpage

1249

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;

fLanguage

English

Publisher

ieee

Conference_Titel

Control, Automation and Systems (ICCAS), 2012 12th International Conference on

Conference_Location

JeJu Island

Print_ISBN

978-1-4673-2247-8

Type

conf

Filename

6393322