FIELD: aircraft engineering.
SUBSTANCE: aircraft fuselage 1 comprises skin element 2 and structural element 7. Intermediate space 5, 9 is arranged between skin element 2 and structural element 2 to receive air carried by airflow 10. Fuselage allows forming airflow 10 to feed air in composed of air inflow/outflow of fuselage sealed inner space 20. Intermediate space 5, 9 is communicated with connection of air inflow/outflow of fuselage sealed inner space 20. Invention covers aircraft with described fuselage. Method is characterised by use of said fuselage.
EFFECT: decreased weight of fuselage active isolation.
13 cl, 9 dwg
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Authors
Dates
2012-11-20—Published
2008-02-21—Filed