FIELD: aviation.
SUBSTANCE: invention relates to landing gear nodes of aircrafts, in particular to landing gear nodes of aircrafts containing a case, inside which a compression link node is placed. The landing gear node for use with the aircraft contains a case, a plunger, and a compression link node. The case contains a cylindrical part, a setting cavity, a connecting element in the form of a roller, the front strut and the rear strut that together form a hole passing through the specified case. The plunger is located inside the specified cavity and is available through the specified hole. The compression link node is connected between the specified plunger and the specified case, located at least partially inside the specified cavity and available through the specified hole.
EFFECT: increase in the construction strength during operation is achieved.
20 cl, 12 dwg
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