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.
Simulation Research on Braking Safety Properties of Aircraft Traction System
Key Engineering Materials ; 419-420 ; 705-708
08.10.2009
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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