发明名称 ジェットエンジン
摘要 PROBLEM TO BE SOLVED: To achieve a simple and lightweight inlet structure of a jet engine.SOLUTION: A jet engine includes an inlet that is formed between first and second cowls. When seen along an air stream flowing into the inlet, a tip of the first cowl is positioned on an upstream side with respect to a tip of the second cowl. A tip part of the second cowl is a disappearance part that disappears with time during flight.
申请公布号 JP6016616(B2) 申请公布日期 2016.10.26
申请号 JP20120279664 申请日期 2012.12.21
申请人 三菱重工業株式会社 发明人 上野 祥彦;古谷 正二郎
分类号 F02C7/042;F02C7/00;F02K7/10 主分类号 F02C7/042
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