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发明名称
BYPASS TURBOJET ENGINE
摘要
A bypass turbojet engine includes a subsonic intake, compressors and turbines of low, medium and high pressure, combustion chamber, outlet nozzles. The engine includes impellers and fixed guide apparatuses.
申请公布号
UA66620(U)
申请公布日期
2012.01.10
申请号
UA20110007780U
申请日期
2011.06.20
申请人
ZAPORIZHIA NATIONAL TECHNICAL UNIVERSITY
发明人
MAMEDOV BORYS SHAMSHADOVYCH
分类号
F02C7/04;F04D27/02
主分类号
F02C7/04
代理机构
代理人
主权项
地址
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