FIELD: transport.
SUBSTANCE: invention relates to aircraft landing gear and concerns multiwheel bogies. The landing gear contains landing gear bogie beam, landing gear leg the first end of which is pivotally connected with aircraft and the second end is pivotally connected with landing gear bogie beam, and stop. The stop is made capable to limit landing gear bogie beam rotation relative to landing gear leg. The stop contains elongated element made capable to deviate in bending when landing gear bogie beam reaches maximum angle of rotation.
EFFECT: absorption of high energies during excessive turn of landing gear bogie beam, higher degree of bogie beam energy dissipation control.
16 cl, 10 dwg
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