Evaluation of the Friction Coefficient from the Dynamometer Test of the Aircraft

  • Woo, Gui-Aee (Machine Control & Application Research Group, Korea Electrotechnology Research Institute) ;
  • Jeon, Jeong-Woo (Machine Control & Application Research Group, Korea Electrotechnology Research Institute) ;
  • Lee, Ki-Chang (Machine Control & Application Research Group, Korea Electrotechnology Research Institute) ;
  • Kim, Yong-Joo (Machine Control & Application Research Group, Korea Electrotechnology Research Institute)
  • Published : 2003.10.22

Abstract

In the braking system, the friction force is the most important factor of the design. For long time, many researchers have been strived for getting the exact friction coefficients. But the friction coefficients are affected by the road condition and changed by lots of parameters, such as normal force and characteristics between two contacted materials, temperature, etc. For the development of ABS of the aircraft, HILS(Hardware-In-the-Loop-Simulation) test and dynamometer test was carried out. For the calculation of the friction coefficients, the wheel moments were measured using the load cell mounted on the housing of the wheel. The test conditions were dry and greasy, as the 0.7 and 0.4 in friction coefficient, respectively. In this paper, the test results of the friction coefficients were represented and the improvement method was suggested.

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