Processing of polymer‐derived, aerogel‐filled, SiC foams for high‐temperature insulation

Author:

Zambotti Andrea1ORCID,Ionescu Emanuel23ORCID,Gargiulo Nicola4ORCID,Caputo Domenico45,Vakifahmetoglu Cekdar6ORCID,Santhosh Balanand1ORCID,Biesuz Mattia1ORCID,Sorarù Gian Domenico17ORCID

Affiliation:

1. Department of Industrial Engineering Glass and Ceramics Laboratory University of Trento Trento Italy

2. Institute of Materials Science Darmstadt University of Technology Darmstadt Germany

3. Fraunhofer Research Institution for Materials Recycling and Resource Strategy Alzenau Germany

4. Center for Advanced Metrological and Technological Services (CeSMA) Federico II University of Naples Napoli Italy

5. Department of Chemical Materials and Industrial Production Engineering Federico II University of Naples Napoli Italy

6. Department of Materials Science and Engineering Izmir Institute of Technology Izmir Turkey

7. National Research Council Italy ICMATE CNR Institute of Condensed Matter Chemistry and Technologies Energy Genoa Italy

Abstract

AbstractPorous polymer‐derived ceramics (PDCs) are outperforming materials when low‐density and thermal inertia are required. In this frame, thermal insulating foams such as silicon carbide (SiC) ones possess intriguing requisites for aerospace applications, but their thermal conductivity is affected by gas phase heat transfer and, in the high temperature region, by radiative mechanisms. Owing to the versatility of the PDC route, we present a synthesis pathway to embed PDC SiC aerogels within the open cells of a SiC foam, thus sensibly decreasing the thermal conductivity at 1000°C from 0.371 W·m−1K−1 to 0.243 W·m−1K−1. In this way, it was possible to couple the mechanical properties of the foam with the insulating ability of the aerogels.The presented synthesis was optimized by selecting, among acetone, n‐hexane, and cyclohexane, the proper solvent for the gelation step of the aerogel formation to obtain a proper mesoporous colloidal structure that, after ceramization at 1000°C, presents a specific surface area of 193 m2·g−1. The so‐obtained ceramic composites present a lowest density of 0.18 g·cm−3, a porosity of 90% and a compressive strength of 0.76 MPa.

Funder

Air Force Office of Scientific Research

Publisher

Wiley

Subject

Materials Chemistry,Ceramics and Composites

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