Insulation of an aircraft fuselage structure

Details Insulation of an aircraft fuselage structure Insulation of an aircraft fuselage structure

B - Operations, Transporting

64

C

B64C 1/40 (2006.01) B64C 1/12 (2006.01)

Patent

CA 2648858

The present invention pertains to a specially designed insulating mat (1) for the sound insulation of an aircraft fuselage structure that is composed of frames (4) and stringers (3) extending transverse to the frames (4), to a specially designed fastening means (8) for fastening an insulating mat (1) on an aircraft fuselage structure such that acoustic bridges are prevented, and to an insulating kit (1, 8) that comprises at least one inventive insulating mat (1) as well as at least one inventive fastening means (8). The insulating mat (1) features a multitude of fastening clips (17) that are fixed on a first surface of the insulating mat (1) and laterally protrude over the border of the insulating mat (1).

La présente invention concerne un tapis isolant (1) spécialement conçu pour l'isolation sonore d'une structure de fuselage d'avion qui est composé de châssis (4) et de lisses (3) s'étendant transversalement par rapport aux châssis (4) ; un moyen de fixation (8) spécialement conçu pour fixer un tapis isolant (1) sur une structure de fuselage d'avion de sorte à empêcher des ponts sonores ; et un ensemble d'isolation (1, 8) qui comprend au moins un tapis isolant inventif (1) ainsi qu'au moins un moyen de fixation inventif (8). Le tapis isolant (1) présente une multitude de pinces de fixation (17) qui sont fixées sur une première surface du tapis isolant (1) et qui dépassent latéralement au-delà du bord du tapis isolant (1).

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