发明名称 Jet flow nozzle and jet engine
摘要 The present invention relates to a jet engine including protrusions (1) for preventing the increase of the velocity gradient of a fluid in a mixed layer of a jet flow and an external air flow by bending the mixed layer, when viewed from the side of a jet flow injected.
申请公布号 US9140210(B2) 申请公布日期 2015.09.22
申请号 US201013639621 申请日期 2010.10.20
申请人 IHI CORPORATION 发明人 Oba Yoshinori;Oishi Tsutomu;Tanaka Nozomi;Kusuda Shinya
分类号 F02K1/08;F02K1/38;F02K1/46;F02K1/48;F02C7/00;F02C7/045 主分类号 F02K1/08
代理机构 Ostrolenk Faber LLP 代理人 Ostrolenk Faber LLP
主权项 1. A jet flow nozzle which is mounted on a jet engine and injects a jet flow to an outside, the jet flow nozzle comprising: a nozzle outlet end that injects the jet flow, wherein the jet flow comprises a fan bypass airflow and a core exhaust airflow; protrusions that are provided around the nozzle outlet end, wherein the protrusions have a triangular pyramid shape that protrudes radially toward a center of the nozzle outlet end, wherein each protrusions has a height of 2.5 to 3.0% of a diameter of the nozzle outlet end.
地址 JP