FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft power plant. Power plant comprises turbojet 2 including fan case 12, mid case 21 fitted radially inside said fan case, central housing 16, circular structure 60 covering said central housing 14 and coupled with the latter by intermediate fasteners 62. Reinforcing structure 64a, 64b is coupled with first and second assemblies 6a, 6b to form shift plane and rigidly mounted at circular structure at first attachment point 68a, 68b, on fan case at second attachment point 70a, 70b and on structural link 17 or mid case 21 at third attachment point 72a, 72b. Reinforcing structure 64a, 64b is located in imaginary plane 66a, 66b parallel turbojet axis 5 or crossing said axis as well as crossing turbojet front assembly attachment point 61a, 61b on fan case 12.
EFFECT: ruled pout deformation of fan case and turbojet central housing.
9 cl, 15 dwg
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