FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft engine mount including engine suspension system 11. Proposed structure comprises thrust transfer device 9 furnished with two lateral links 90 and cross-arm 91 arranged at support 42 and jointed thereto by cross-arm primary connector 100 to make cross-arm hinge axle 104 located in plane P. Said cross-arm is fitted at said support 42 using cross-arm secondary connector 108 located at certain distance from said primary connector 100, if seen from top to make cross-arm secondary hinge axle (PO) located also in said plane P. In compliance with this invention, turning of said cross-arm is interrupted when device 108 gets in contact with cross-arm.
EFFECT: simplified design, decreased overall dimensions.
10 cl, 7 dwg
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