Method for manufacturing cabin panels for aircraft propulsion components

摘要

The invention relates to a method for manufacturing a panel, which comprises a honeycomb structure forming a cavity and a first skin () 31 and a second skin () 32, the second skin covering the honeycomb structure. The method includes the step of placing one or more supports in a corresponding cavity of the honeycomb structure. These carriers (4) are made of escape materials such as thermoplastic. According to the invention, the carrier ((4) is heated, so that the size between the first () 31 and the second skin ((32) is less than a predetermined value under the influence of increased temperature.