FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft undercarriage, undercarriage load reaction unit, and to method of controlling load at undercarriage. Undercarriage comprises shock strut with top and bottom telescoping sections. Note here that top section is connected to airframe. It comprises also lever extending to and fro relative to aircraft to support undercarriage wheel and articulated with shock strut bottom section via main pivot pin. Besides, undercarriage comprises load reaction unit and landing load control indicator.
EFFECT: control over load at undercarriage at landing.
31 cl, 7 dwg
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