Investigation of the impact of a particle foam insulation on frost buildup on the aircraft structure

• Published in: IOP conference series. Materials Science and Engineering Vol. 1226; no. 1; pp. 12054 - 12061
• Main Authors: Norrefeldt, Victor, Riedl, Gerhard
• Format: Journal Article
• Language: English
• Published: Bristol IOP Publishing 01.02.2022
• Subjects: Aircraft; Aircraft compartments; Aircraft structures; Cold; Cold surfaces; Feasibility studies; Glass fibers; Indoor environments; Insulation; Pressure effects
• ISSN: 1757-8981; 1757-899X
• DOI: 10.1088/1757-899X/1226/1/012054

Abstract The aircraft insulation separates the thermally comfortable cabin interior environment from the extremely cold outside condition. However, the fabrication and installation of the insulation in the aircraft is a labour intensive task. Tailored, rigid particle foam parts could be a solution to speed up installation process. The presented study investigates the feasibility of such a concept from a hygrothermal point of view. Due to the temperature difference between the cold air trapped between aircraft skin and insulation on one side and the warm cabin air on the other side, a buoyancy induced pressure difference forms. This effect drives the warmer air through leakages in the insulation system towards the cold skin. Here, moisture contained in the air condenses on the cold surfaces, increasing the risk for uncontrolled dripping (“rain in the plane”) when it melts. Therefore, this study compares the frost build-up of different installations of a rigid particle foam frame insulation with the classical glass fiber capstrip. Tests are hosted in the Fraunhofer Lining and Insulation Test Environment chamber.