Jet fuel oxidation on conventionally and additively manufactured metallic tubes
• High heat loads can cause jet fuel to crack and foul at elevated temperatures. • Jet fuel coking on additively manufactured tubes is studied. • Surface roughness associated with 3D printing deteriorates the fouling behavior. • Application of suitable surface coating helps to mitigate unwanted fouling. In the aviation industry, jet fuel is a propellant as well as a coolant. At elevated temperatures, the jet fuel experiences significant thermal stresses, which leads to the oxidation of hydrocarbons when exposed to the heat exchanger walls. As a result, undesirable insoluble carbon deposits on the internal heat exchanger walls impede the effectiveness of the heat exchanger and the aircraft fuel circulatory system, compromising aircraft safety and performance. Here, we study the jet fuel fouling behavior on additively manufactured tubes created using stainless steel, aluminum alloy, titanium, and Inconel, during autoxidation at elevated temperatures. Additively manufactured materials are tested due to their numerous potential benefits for the aerospace industry, which include design flexibility for the creation of complex and optimized parts that enhance performance and aerodynamics. Experiments were conducted using a fuel-fouling open loop system based on the Jet Fuel Thermal Oxidation Test (JFTOT). Scanning electron microscopy and characterization of the internal surface of the tubes showed that the jet fuel reacts differently with different metals and alloys. Comparisons were made with traditionally manufactured materials and benchmarked with the performance of bare copper tubes. We show that additively manufactured tubes were more prone to fuel fouling due to the larger inherent roughness associated with the additive manufacturing process. We show that applying a thin layer of commercially available Silcolloy 2000 coating onto the internal surface minimizes jet fuel degradation significantly. Our work helps to enable the application of additive manufacturing for aircraft thermal management component manufacture by alleviating concerns related to fuel blockage and performance deterioration stemming from surface deposition.
Authors
- Nenad Miljkovic (ORCID: https://orcid.org/0000-0002-0866-3680)
- Kazi Fazle Rabbi (ORCID: https://orcid.org/0000-0003-3630-1625)
- Mohammed Jubair Dipto
- Tarandeep Singh Thukral (ORCID: https://orcid.org/0009-0000-0158-3218)
Institutions
- Kyushu University (JP)
- University of Illinois Urbana-Champaign (US)
Publication Details
- Journal
- Applied Thermal Engineering
- Published
- 2024-12-04
- DOI
- https://doi.org/10.1016/j.applthermaleng.2024.125155
- Citations
- 5
- Primary Topic
- Rocket and propulsion systems research
- Type
- article
- Field-Weighted Citation Impact
- 6.49
Funders
- National Science Foundation
- Air Conditioning and Refrigeration Center
- Ministry of Education, Culture, Sports, Science and Technology
- International Institute for Carbon-Neutral Energy Research, Kyushu University