Please use this identifier to cite or link to this item: http://hdl.handle.net/11455/2501
DC FieldValueLanguage
dc.contributor.advisor李興軍zh_TW
dc.contributor.advisorLee Hsing Juinen_US
dc.contributor.author林南宏zh_TW
dc.contributor.authorHung, Lin Nanen_US
dc.date1994zh_TW
dc.date.accessioned2014-06-05T11:43:27Z-
dc.date.available2014-06-05T11:43:27Z-
dc.identifier.urihttp://hdl.handle.net/11455/2501-
dc.description.abstract與渦輪軸引擎比較,往復式內燃機有一些潛在的缺失,例如:熱效率不高又 難以提昇,馬力重量比低,機件較複雜,動平衡較困難,運轉壽限短,燃料可 容性低等問題.然而航空或地面車輛用渦輪軸引擎雖有較佳之機械性能,但 其渦輪葉片卻須承受高溫,高轉速之工作環境下所引致之熱應力,高離心 力,疲勞,破壞,潛變,冷卻等等問題,其材質,加工製造,品管要求均極為嚴 苛.若渦輪噴射引擎能於動力輸出上不使用渦輪葉片,對於成本降低,可靠 度提昇等方面均有重大之意義.有鑑於此,本文特提出一釜底抽薪之計,採 無葉片式之旋噴機構來取代渦輪葉片,以輸出噴射引擎之動力,整合設計成 一新潁的旋噴式噴射引擎.zh_TW
dc.language.isoen_USzh_TW
dc.publisher機械工程研究所zh_TW
dc.subjectsprinkleren_US
dc.subject旋噴機構zh_TW
dc.subjectducted fanen_US
dc.subjectturbojet engineen_US
dc.subject導風扇zh_TW
dc.subject渦輪噴射引擎zh_TW
dc.title旋噴式導風扇引擎暨渦輪噴射引擎之先導設計與測試zh_TW
dc.titlePreliminary Design and Performance Test of cted Fan-Sprinkler Engine and Turbojet-Sprinkler Engineen_US
dc.typeThesis and Dissertationzh_TW
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.openairetypeThesis and Dissertation-
item.cerifentitytypePublications-
item.fulltextno fulltext-
item.languageiso639-1en_US-
item.grantfulltextnone-
Appears in Collections:機械工程學系所
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