Abstract: A climate tube, in particular for aircraft, includes an inner layer and an outer layer of fiber composite plastic material. To achieve a high stiffness combined with a low weight and to achieve good thermal insulation properties, disposed between the inner layer and the outer layer is an at least almost completely circumferential honeycomb core, which is firmly connected to the inner layer the outer layer. The radial extent of the honeycomb core is large compared to the radial extent of the inner layer and the outer layer, and the mutually opposed longitudinal ends of the honeycomb core abut one another and are surrounded by a ply of fiber composite plastic material.

Abstract: The invention relates to a climate tube (10), in particular for aircraft, having an inner layer (12) and an outer layer (16) of fiber composite plastic material. To achieve a high stiffness combined with a low weight and to achieve good thermal insulation properties, disposed between the inner layer (12) and the outer layer (16) is an at least almost completely circumferential honeycomb core (14), which is firmly connected to the inner layer (12) and the outer layer (16) and the radial extent of which is large compared to the radial extent of the inner layer (12) and the outer layer (16).