M. Burston, Tim Conroy, Luke Spiteri, M. Spiteri, C. Bil, G. Dorrington
{"title":"Conceptual Design of Sustainable Liquid Methane Fuelled Passenger Aircraft","authors":"M. Burston, Tim Conroy, Luke Spiteri, M. Spiteri, C. Bil, G. Dorrington","doi":"10.3233/978-1-61499-302-5-391","DOIUrl":null,"url":null,"abstract":"Motivated by concerns over rising costs of Jet-A fuel and the current limitations of \"drop-in\" fuel substitutes, it is proposed that biomethane (or Bio- LNG) provides a promising sustainable aviation fuel. This paper discusses some technical considerations for converting a jet airliner to biomethane fuel. Following consideration of aircraft configuration alternatives and performance issues, a conceptual design is presented where cryogenic methane is stored in both an insulated wing-box and under-wing pods. It is concluded that the weight penalty of such a cryogenic fuel system would be relatively modest, hence the range and payload capability of existing Jet-A aircraft can be matched.","PeriodicalId":213842,"journal":{"name":"ISPE International Conference on Concurrent Engineering","volume":"16 3 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"7","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"ISPE International Conference on Concurrent Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.3233/978-1-61499-302-5-391","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 7
Abstract
Motivated by concerns over rising costs of Jet-A fuel and the current limitations of "drop-in" fuel substitutes, it is proposed that biomethane (or Bio- LNG) provides a promising sustainable aviation fuel. This paper discusses some technical considerations for converting a jet airliner to biomethane fuel. Following consideration of aircraft configuration alternatives and performance issues, a conceptual design is presented where cryogenic methane is stored in both an insulated wing-box and under-wing pods. It is concluded that the weight penalty of such a cryogenic fuel system would be relatively modest, hence the range and payload capability of existing Jet-A aircraft can be matched.