INSULATING ARRANGEMENT FOR THE INNER INSULATION OF AN AIRCRAFT
摘要
The invention relates to an insulating arrangement for the inner insulation of an aircraft according to the preamble of claim 1. Appropriate measures (and control of ventilation) ensure that almost no humid air or other humid gas o r water (vapor) particles penetrate a film-covered insulating packet (1) while the accumulated humidity will quickly and easily escape (if such accumulatio n has taken place) from the insulating packet (1). The insulating arrangement consists of an insulating packet (1) which is covered by a film (4). The fil m is arranged within a clearance (7) between an inner insulation (12) and a shell (6). The insulating packet (1) which is completely covered by the film (4) does not line the clearance (7) entirely. The film consists of a gas- permeable film material which permits realization of different diffusion resistance behaviors depending on the direction of diffusion of the entire structure.