Simulation Research on Braking Safety Properties of Aircraft Traction System

Neng Jian Wang; Li Jie Zhou; Qiang Song; De Fu Zhang

doi:10.4028/www.scientific.net/KEM.419-420.705

Paper Titles

A Formal EXPRESS-to-OWL Mapping Algorithm
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Simulation of Diesel Electronic Control PPVI Fuel Injection System
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Research on Simulation System of the Interfacing Apparatus of Underwater Vehicle Based on VR
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An Intelligent Image Segmentation Algorithm for Medical Ultrasonic Instruments
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Simulation Research on Braking Safety Properties of Aircraft Traction System
p.705

Solution of the Edges of Mode III Asymmetrical Dynamic Interface Crack Subjected to Variable Loads
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Hardware-in-the-Loop Simulation of Speed-Adjusting System for DC Motor Based on dSPACE
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Study of Ship Motion Simulation Based on HLA Technology
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A Methodology to Estimate the Reliability of Passageway system in Naval Ship Design
p.721

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Simulation Research on Braking Safety Properties of Aircraft Traction System

Abstract:

The jack-knifing tendency of aircraft traction system during braking was discussed and analyzed using multi-body dynamics models that consist of aircraft-towing tractor, aircraft draw link and aircraft. The braking critical conditions of the aircraft traction system for straight-line braking and turning braking were discussed and analyzed respectively. In the case of straight-line braking, the effect of friction coefficient on the maximum braking torque is described. In the case of turning braking, the relationship between the maximum baking torque and relative angle is obtained.