| 摘要 |
The present invention relates to a fuselage (1) of an aircraft or spacecr aft, with at least one shell element (2) and a structural element (7). An in terspace (5; 9) to which air can be admitted by an air stream (10) is provid ed between the at least one shell element (2) and the structural element (7) . The fuselage is distinguished by the fact that, to form the air-admitting air stream (10) as an outgoing/incoming air stream of a pressurized interior space (20) of the fuselage (1), the interspace (5; 9) is connected to a cor responding outgoing/ incoming air connection of the interior space (20). The invention also relates to a corresponding aircraft or spacecraft and to a m ethod of actively insulating such a fuselage (1). |
