FIELD: engines and pumps.
SUBSTANCE: bypass turbojet engine for attachment on side of fuselage by means of spaced apart in longitudinal direction of front and rear suspensions comprises intermediate housing outer shell attached to front suspension and thrust main structure attached to rear suspension. Intermediate housing outer shell and main structure are retained coaxial with help of set of pins, each of which is hollow in cross section and is attached by their ends to shell and main structure. Pins are made and/or arranged to be deformed in response to turbojet engine thrust by creating deforming moment between shell and main structure. Deforming moment has opposite tension, which is created under action of same turbojet thrust lever arm between axis of thrust and front suspension. Another invention relates to intermediate housing, made to be attached to above engine and containing outer shell and pins, which are suitable for connection of outer shell with thrust of main structure.
EFFECT: group of inventions allows reducing weight of jet turbine engine.
9 cl, 7 dwg
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