Nacelle air intake structure

Details Nacelle air intake structure Nacelle air intake structure

B - Operations, Transporting

64

D

B64D 29/00 (2006.01) B64D 29/08 (2006.01)

Patent

CA 2736594

The invention relates to a nacelle comprising an air intake structure (1) able to channel a flow of air towards a fan of the turbojet engine, said structure (1) comprising at least one inner panel (11) and one outer panel (10), the outer panel (10) being able to be moved by guide means (30) so as to open up the air intake structure (1), characterized in that it further comprises means (40, 60) for protecting the inner panel (11) against fire, said means being able to be moved in whole or in part when the air intake structure (1) is opened.

L'invention concerne une nacelle comprenant une structure d'entrée d'air (1) apte à canaliser un flux d'air vers une soufflante de tarboréacteur, ladite structure (1) comprenant au moins un panneau interne (11) et un panneau externe (10), le panneau externe (10) étant apte à être déplacé par des moyens de guidage (30) de manière à ouvrir la structure d'entrée d'air (1), caractérisé en ce qu'elle comprend, en outre, des moyens (40,60) de protection contre le feu du panneau interne (11), lesdits moyens étant aptes à être déplacés tout ou en partie lors de l'ouverture de la structure d'entrée d'air (1).

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