FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering and can be used in aircraft gas turbine attachments. Proposed device comprises suspension front and rear mounts, one representing a suspension lever with fasteners arranged on its ends pin-jointed to ear made in aircraft engine housing. Suspension lever top part is pivoted to aircraft pylon. Every connecting element of aforesaid suspension lever is directly connected with mating engine eat. Note that at least one lengthwise axis of pivot joints is located across engine lengthwise axis.
EFFECT: reduced suspension sizes.
7 cl, 7 dwg
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