Aircraft Skid Resistance Failure Risk Assessment Based on Virtual Prototype in Wet Sliding State

ZHU Xingyi; WU Yanan; BAI Shunjie; CHEN Long

doi:10.11936/bjutxb2022010008

Journal of Beijing University of Technology > 2022 > 48(6): 644-654. > DOI: 10.11936/bjutxb2022010008

ZHU Xingyi, WU Yanan, BAI Shunjie, CHEN Long. Aircraft Skid Resistance Failure Risk Assessment Based on Virtual Prototype in Wet Sliding State[J]. Journal of Beijing University of Technology, 2022, 48(6): 644-654. DOI: 10.11936/bjutxb2022010008

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Aircraft Skid Resistance Failure Risk Assessment Based on Virtual Prototype in Wet Sliding State

1.
Key Laboratory of Road and Traffic Engineering of Ministry of Education, Tongji University, Shanghai 201804, China
2.
Hangzhou International Airport Co., Ltd., Hangzhou 311207, China
3.
Shanghai Pudong Architectural Design & Research Institute Co., Ltd., Shanghai 201206, China

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Received Date: December 09, 2021
Revised Date: February 20, 2022
Available Online: August 03, 2022
Published Date: June 09, 2022

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Abstract

Abstract

To solve the problem of aircraft landing safety in the wet condition of the runway, the authors used the tire-water film-road surface finite element models as the basis and combined the skid resistance performance of the road surface with the risk assessment of skid resistance failure by means of a virtual prototype to quantitatively assess the risk of aircraft running off the runway. Furthermore, the equivalent adhesion coefficient was proposed, and the three-dimensional surface of "adhesion coefficient-slip rate" under different speeds and different water film states was drawn. Finally, taking the two runways as examples (length 3 600 m and 3 400 m), the risk level of aircraft rushing out of the runway under different water film states was calculated. When the runway was dry, the risk level of the aircraft to rush out of the runway was E, which means there is basically no possibility to rush out of the runway. When the thickness of the water film was 3 mm, the possibility of the aircraft rushing out of the runway rises sharply. Referring to the Federal Aviation Administration (FAA) standard, the risk level at this time was B. However, when calculating the braking distance of the aircraft, the thrust of the aircraft was not considered, therefore the calculation results are generally safe.

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References (27)

References

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Aircraft Skid Resistance Failure Risk Assessment Based on Virtual Prototype in Wet Sliding State

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