FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly to aircraft engine support and method on mounting engine on said support. Aircraft engine support (4) comprises rigid structure (10) that makes box covered by front ring (36) on its front face. Support comprises also engine mounting system (11) attached to rigid structure(10) and, in particular front attachment assemble (6) coupled with main part (46) fixed on rigid structure (10). Said main part (46) is arranged nearby front surface (38) of aforesaid covering rib (36), while front engine attachment (6) incorporates shear pin (68) passing through said main part (46) and front rib (36). To mount engine on support, engine (2) is arranged relative to support to have first primary hole (56) located opposite to second primary hole (58). Then pin (80) with convex centering head (82) is inserted into said primary holes (56, 58) for said pin to make said shear pin (68).
EFFECT: transmission of engine-generated loads and reduce support height.
15 cl, 12 dwg
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