FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to turbine engine suspensions. Claimed bar comprises the first and second attachments. The first attachment is meant for fastening to aircraft structure. The second attachment is meant for fastening to the engine. Said bar is made partially from composite including the fibres for reinforcement of metal matrix and shaped to circle arc.
EFFECT: perfected properties of the suspension.
17 cl, 22 dwg
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