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Experimental study on the accretion and release of ice in aviation jet fuel
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| Veröffentlicht in: | Aerospace science and technology 82/83(2018), Seite 294-303 |
|---|---|
| Personen und Körperschaften: | , , , |
| Titel: | Experimental study on the accretion and release of ice in aviation jet fuel/ Mathias Schmitz, Gerhard Schmitz |
| Format: | E-Book-Kapitel |
| Sprache: | Englisch |
| veröffentlicht: |
2018
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| Gesamtaufnahme: |
: Aerospace science and technology, 82/83(2018), Seite 294-303
, volume:82/83 |
| Schlagwörter: | |
| Quelle: | Verbunddaten SWB Lizenzfreie Online-Ressourcen |
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| 520 | |a Ice formations in aircraft fuel systems pose a serious safety threat with potentially disastrous consequences, when restricting the fuel flow towards the engines. This is an ongoing challenge in the aerospace industry. In this work experimental studies have been performed to investigate the effects of temperature, flow rate and surface properties on the accretion and release of ice in flowing fuel. A test rig with a glass-windowed pipe has been employed to quantitatively measure the transient icing process under controlled conditions. The accreted ice exhibited soft and fluffy characteristics and was most likely the result of impinging solid ice particles that were entrained in the fuel flow. The ice particles were most sticky in a temperature range between −6°C and −20°C. The thickness of accreted ice decreased with roughness on aluminium surfaces and there was a significant reduction on polytetrafluoroethylene (PTFE) and polymethyl methacrylate (PMMA) in comparison to aluminium, copper or stainless steel surfaces. Comparison of the thickness of accreted ice with the ice adhesion strength reported in the literature showed a clear correlation. The experimental results will help to gain better understanding of the ice accretion process in flowing fuel and may serve as basis for design guidelines to minimize ice formation within an aircraft fuel system. | ||
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| author | Schmitz, Mathias, Schmitz, Gerhard |
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| contents | Ice formations in aircraft fuel systems pose a serious safety threat with potentially disastrous consequences, when restricting the fuel flow towards the engines. This is an ongoing challenge in the aerospace industry. In this work experimental studies have been performed to investigate the effects of temperature, flow rate and surface properties on the accretion and release of ice in flowing fuel. A test rig with a glass-windowed pipe has been employed to quantitatively measure the transient icing process under controlled conditions. The accreted ice exhibited soft and fluffy characteristics and was most likely the result of impinging solid ice particles that were entrained in the fuel flow. The ice particles were most sticky in a temperature range between −6°C and −20°C. The thickness of accreted ice decreased with roughness on aluminium surfaces and there was a significant reduction on polytetrafluoroethylene (PTFE) and polymethyl methacrylate (PMMA) in comparison to aluminium, copper or stainless steel surfaces. Comparison of the thickness of accreted ice with the ice adhesion strength reported in the literature showed a clear correlation. The experimental results will help to gain better understanding of the ice accretion process in flowing fuel and may serve as basis for design guidelines to minimize ice formation within an aircraft fuel system. |
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| spelling | Schmitz, Mathias 1983- VerfasserIn (DE-588)1175438030 (DE-627)1046393413 (DE-576)516203363 aut, Experimental study on the accretion and release of ice in aviation jet fuel Mathias Schmitz, Gerhard Schmitz, 2018, Illustrationen, Diagramme, Text txt rdacontent, Computermedien c rdamedia, Online-Ressource cr rdacarrier, Ice formations in aircraft fuel systems pose a serious safety threat with potentially disastrous consequences, when restricting the fuel flow towards the engines. This is an ongoing challenge in the aerospace industry. In this work experimental studies have been performed to investigate the effects of temperature, flow rate and surface properties on the accretion and release of ice in flowing fuel. A test rig with a glass-windowed pipe has been employed to quantitatively measure the transient icing process under controlled conditions. The accreted ice exhibited soft and fluffy characteristics and was most likely the result of impinging solid ice particles that were entrained in the fuel flow. The ice particles were most sticky in a temperature range between −6°C and −20°C. The thickness of accreted ice decreased with roughness on aluminium surfaces and there was a significant reduction on polytetrafluoroethylene (PTFE) and polymethyl methacrylate (PMMA) in comparison to aluminium, copper or stainless steel surfaces. Comparison of the thickness of accreted ice with the ice adhesion strength reported in the literature showed a clear correlation. The experimental results will help to gain better understanding of the ice accretion process in flowing fuel and may serve as basis for design guidelines to minimize ice formation within an aircraft fuel system., Fuel system, Aviation fuel, Low temperatures, Water, Ice accretion, Ice formation, Schmitz, Gerhard 1955- VerfasserIn (DE-588)14162552X (DE-627)630395063 (DE-576)324447833 aut, Technische Universität Hamburg Sonstige Körperschaft 4oth (DE-588)1112763473 (DE-627)866918418 (DE-576)476770564 oth, Technische Universität Hamburg Institut für Technische Thermodynamik Sonstige Körperschaft (DE-588)1126767204 (DE-627)881359149 (DE-576)484783777 oth, Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 82/83(2018), Seite 294-303 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns, volume:82/83 year:2018 pages:294-303, https://doi.org/10.1016/j.ast.2018.08.034 Resolving-System Volltext, http://nbn-resolving.de/urn:nbn:de:gbv:830-882.025653 Resolving-System kostenfrei Volltext, https://doi.org/10.15480/882.1972 Resolving-System kostenfrei Volltext, http://hdl.handle.net/11420/1975 Resolving-System kostenfrei Volltext, http://nbn-resolving.de/urn:nbn:de:gbv:830-882.025653 LFER, LFER 2019-05-29T00:00:00Z |
| spellingShingle | Schmitz, Mathias, Schmitz, Gerhard, Experimental study on the accretion and release of ice in aviation jet fuel, Ice formations in aircraft fuel systems pose a serious safety threat with potentially disastrous consequences, when restricting the fuel flow towards the engines. This is an ongoing challenge in the aerospace industry. In this work experimental studies have been performed to investigate the effects of temperature, flow rate and surface properties on the accretion and release of ice in flowing fuel. A test rig with a glass-windowed pipe has been employed to quantitatively measure the transient icing process under controlled conditions. The accreted ice exhibited soft and fluffy characteristics and was most likely the result of impinging solid ice particles that were entrained in the fuel flow. The ice particles were most sticky in a temperature range between −6°C and −20°C. The thickness of accreted ice decreased with roughness on aluminium surfaces and there was a significant reduction on polytetrafluoroethylene (PTFE) and polymethyl methacrylate (PMMA) in comparison to aluminium, copper or stainless steel surfaces. Comparison of the thickness of accreted ice with the ice adhesion strength reported in the literature showed a clear correlation. The experimental results will help to gain better understanding of the ice accretion process in flowing fuel and may serve as basis for design guidelines to minimize ice formation within an aircraft fuel system., Fuel system, Aviation fuel, Low temperatures, Water, Ice accretion, Ice formation |
| title | Experimental study on the accretion and release of ice in aviation jet fuel |
| title_auth | Experimental study on the accretion and release of ice in aviation jet fuel |
| title_full | Experimental study on the accretion and release of ice in aviation jet fuel Mathias Schmitz, Gerhard Schmitz |
| title_fullStr | Experimental study on the accretion and release of ice in aviation jet fuel Mathias Schmitz, Gerhard Schmitz |
| title_full_unstemmed | Experimental study on the accretion and release of ice in aviation jet fuel Mathias Schmitz, Gerhard Schmitz |
| title_in_hierarchy | Experimental study on the accretion and release of ice in aviation jet fuel / Mathias Schmitz, Gerhard Schmitz, |
| title_short | Experimental study on the accretion and release of ice in aviation jet fuel |
| title_sort | experimental study on the accretion and release of ice in aviation jet fuel |
| title_unstemmed | Experimental study on the accretion and release of ice in aviation jet fuel |
| topic | Fuel system, Aviation fuel, Low temperatures, Water, Ice accretion, Ice formation |
| topic_facet | Fuel system, Aviation fuel, Low temperatures, Water, Ice accretion, Ice formation |
| url | https://doi.org/10.1016/j.ast.2018.08.034, http://nbn-resolving.de/urn:nbn:de:gbv:830-882.025653, https://doi.org/10.15480/882.1972, http://hdl.handle.net/11420/1975 |
| urn | urn:nbn:de:gbv:830-882.025653 |