Turboreactor for aircraft

Details Turboreactor for aircraft Turboreactor for aircraft

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/14 (2006.01) F02K 3/04 (2006.01)

Patent

CA 2655424

The invention relates to a turboreactor (100) for an aircraft comprising an engine (103) housed in a nacelle (101) and a heat exchanger (107) intended for cooling a fluid contributing to the propellant system of the engine. The heat exchanger is placed at the level of the outer wall (105) of the engine, an interstitial space wherein the air may circulate being arranged between the outer wall of the engine and an inner wall (112) of the heat exchanger. The invention also relates to an aircraft provided with at least one such turboreactor.

L'invention concerne un turboréacteur (100) pour aéronef comportant un moteur (103) logé dans une nacelle (101) et un échangeur thermique (107) destiné a refroidir un fluide participant au système propulsif du moteur. L' échangeur thermique est disposé au niveau de la paroi externe (105) du moteur, un espace interstitiel dans lequel de l'air peut circuler étant ménagé entre la paroi externe du moteur et une paroi inférieure (112) de l' échangeur thermique. L'invention concerne également un aéronef muni d'au moins un tel turboréacteur.

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