FIELD: aircraft engineering.
SUBSTANCE: turbojet nacelle 1 comprises rear section 6 with internal fixed structure 9 arranged around engine compartment rear to make calibrated outlet section 10 together with jet nozzle 6 with the help of separators arranged in outlet section. Said separators are divided into stiff separators 11, 12 to ensure constant spacing and compensators 13 of relative displacements of turbojet and nacelle. Said compensators consist of a set of elements. One end of said elements is secured to stiff separators while another one is free.
EFFECT: reduced stress at nacelle.
10 cl, 6 dwg
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