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Inner partition and outer panel assembly for air inlet structure of nacelle of turbojet engine of aircraft, has connecting element comprising structural skin fixed to partition and porous material attached to skin and fixed to outer panel
Inner partition and outer panel assembly for air inlet structure of nacelle of turbojet engine of aircraft, has connecting element comprising structural skin fixed to partition and porous material attached to skin and fixed to outer panel
The assembly has a connecting element (19) for connecting components e.g. inner partition (9) and outer panel (3), together, where the device maintains integrity of the surface of the panel. The element has a structural skin (21) fixed to the partition and a porous material (23) attached to the structural skin and fixed to the panel by contact. The porous material is chosen from a group consisting of foam, polystyrene felt and aggregates of small sized components. The skin extends across the porous material and includes ends fixed on the panel through gluing or brazing. An independent claim is also included for an air inlet structure of nacelle of turbojet engine, comprising an inner partition connecting air inlet lever to outer panel.
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