Insulation for pipes, in particular for pipes of a pneumatic system in a commercial aircraft

An insulation assembly for tubes, in particular for pipes of a pneumatic system in a commercial aircraft, has essentially at least an insulating layer and a film made of titanium outer shell. The invention consists in that the outer shell is connected in a first end portion and a second end portion each having a Abschlussprofikl and a shell having at least one longitudinal seam is formed in the insulating layer can be inserted. This has the advantage that the insulation is easy to manufacture in a pre-assembly and installation on the pneumatic pipe system can be done quickly and easily. The light and heat-resistant design of the insulating arrangement allows the use in the pneumatic system of an aircraft. With the intended shell technology, the insulation can be removed separately and, if necessary, damaged insulation parts can be replaced uncomplicated.