FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Nacelle comprises rear section 11 made up of two halves 13a, 13b to confine central section C accommodating turbojet engine 6, annular cold air duct 31 arranged around said section C, one six-hour section 15 arranged under said section C. Nacelle rear section comprises, at least, one pipeline 29a, 29b to communicate said annular duct 31 with said six-hour section 15 to keep relatively low temperature therein. Nacelle rear section comprises also locks 27 to joint halves 13a, 13b together, six-hour section pressure release flaps 17, and grid-type thrust reversal means.
EFFECT: nacelle rear section cooling.
9 cl, 3 dwg
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