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 |