FIELD: attachment units of aircraft power plants.
SUBSTANCE: part 1 of engine mount has ends for holding connecting rods 8 and 9 articulated with turbo-jet engine 3 forming pair of eyes 5 separated by slot 19 made in part 1 to avoid propagation of fatigue cracks 20. Attachment units 11 having cap nuts 13 are located in widened sections 15 of eyes 5 above connecting rods 8 and 9, thus ensuring static strength of eyes 5 when one of them is defective. Provision is also made for reduction of moment created by projection between attachment units 11 and connecting rods 8 and 9.
EFFECT: enhanced safety of engine mount part with no change in dimensions and mass.
2 cl, 1 dwg
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