Aircraft with an insulation system for thermal and acoustic...

Details Aircraft with an insulation system for thermal and acoustic... Aircraft with an insulation system for thermal and acoustic...

B - Operations, Transporting

64

C

B64C 1/40 (2006.01) F16L 59/02 (2006.01) G10K 11/16 (2006.01)

Patent

CA 2755378

The invention relates to an aircraft (100) with an insulation system (101) for thermal insulation and acoustic insulation, with a cabin (102), an outer skin (103), an acoustic insulation unit (104) and a thermal insulation unit (105). The acoustic insulation unit (104) is designed for acoustically insulating the aircraft (100). The thermal insulation unit (105) is designed for thermally insulating the aircraft (100). The acoustic insulation unit (104) and the thermal insulation unit (105) are arranged between the cabin (102) and the outer skin (103).

L'invention concerne un aéronef (100) comportant un système d'isolation (101) destiné à l'isolation thermique et acoustique, l'aéronef comprenant une cabine (102), une peau extérieure (103), une unité d'isolation acoustique (104) et une unité d'isolation thermique (105). L'unité d'isolation acoustique (104) est conçue pour insonoriser l'aéronef (100). L'unité d'isolation thermique (105) est conçue pour isoler thermiquement l'aéronef (100). L'unité d'isolation acoustique (104) et l'unité d'isolation thermique (105) sont disposées entre la cabine (102) et la peau extérieure (103).

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