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CAI Jing, ZHANG Heng, LI Yue, SUN Rui-qiang. Influence of unbalanced pavement friction on landing taxiing parameters of aircraft[J]. Journal of Traffic and Transportation Engineering, 2018, 18(5): 12-24. doi: 10.19818/j.cnki.1671-1637.2018.05.002
Citation: CAI Jing, ZHANG Heng, LI Yue, SUN Rui-qiang. Influence of unbalanced pavement friction on landing taxiing parameters of aircraft[J]. Journal of Traffic and Transportation Engineering, 2018, 18(5): 12-24. doi: 10.19818/j.cnki.1671-1637.2018.05.002
shu

Influence of unbalanced pavement friction on landing taxiing parameters of aircraft

doi: 10.19818/j.cnki.1671-1637.2018.05.002
  • 1.

    Airport College, Civil Aviation University of China, Tianjin 300300, China

  • 2.

    Department of Airport Management, Shanghai Civil Aviation College, Shanghai 200232, China

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  • Author Bio:

    CAIJing(1975-), female, associate professor, PhD, caijing75@163.com

  • Received Date: 2018-04-21
  • Publish Date: 2018-10-25
    Abstract
  • A mechanical model of aircraft landing taxiing was established based on the kinematics principle, and the unbalanced pavement friction degree was introduced.On the basis of the in-situ measured pavement friction coefficient and unbalanced friction degree, the variation tendencies of an aircraft's yaw angle and yaw distance during its landing deceleration and taxiing at constant speed were analyzed.The model tests were conducted, and the variation tendencies of landing taxiing parameters under unbalanced pavement friction of a wet runway were analyzed.Analysis result indicates that the unbalanced runway friction at two sides of a runway centerline leads to the aircraft turning around the vertical axis, which leads to the incurrence of yaw angle and yaw distance during aircraft landing taxiing.Increasing unbalanced pavement friction degree causes an increase in yaw angle and yaw distance during aircraft landing taxiing.When the unbalanced friction degree increases from 0.03 to 0.38, the yaw angle increases by 4 times, and the yawdistance increases by 1 time.Therefore, decreasing unbalanced friction degree at two sides of a runway centerline can effectively reduce the probability of an aircraft's runway deviation in landing taxiing.The slip ratio of tires on the aircraft has little influence on yaw angle and distance of the aircraft.When the pavement friction coefficient decreases, the taxiing distance of deceleration increases linearly.With the increase of unbalanced friction degree on the runway's landing strip, the yaw angle increases linearly.As the unbalanced friction degree reaches 0.165, the yaw angle is 1.2°.With the increases of unbalanced friction degree on the runway's landing strip, the yaw distance also increases.For the yaw angle occurring in deceleration taxiing and a long uniform velocity taxiing distance, above 70% yaw distance in landing taxiing occurrs in the uniform section.When the water film thickness difference on the two sides of wet runway center line increases, the yaw angle and yaw distance during the aircraft's landing taxiing increase as well, and as the water film thickness difference increases from 0.05 mm to 2.50 mm, the yaw angle increases by 6 times, and the yaw distance increases by 5 times.Therefore, the balance of friction at the position of the aircraft's main landing gear on the landing strip should be guaranteed, because it is beneficial to the yaw angle control during an aircraft's deceleration section.

     

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