| 发明名称 |
JET ENGINE, FLYING OBJECT AND METHOD OF OPERATING JET ENGINE |
| 摘要 |
The jet engine includes an inlet and a combustor. The inlet (11) takes air. The combustor burns fuel with the air. The combustor includes an injector (20). The injector (20) has an opening (31) through which the fuel is injected. The injector (20) includes a self-extinguishing member (32). The self-extinguishing member (32) self-extinguishes with time in a flight so that the injection direction of the fuel is modified. |
| 申请公布号 |
US2017067637(A1) |
申请公布日期 |
2017.03.09 |
| 申请号 |
US201515123431 |
申请日期 |
2015.02.18 |
| 申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
UENO Yoshihiko;FURUYA Shojiro |
| 分类号 |
F23R3/28;F02K7/18;F23R3/10 |
主分类号 |
F23R3/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A jet engine, comprising:
an inlet taking air; and a combustor burning fuel with the air, wherein the combustor includes:
an injector having an opening through which the fuel is injected, wherein the injector includes a self-extinguishing member which self-extinguishes with time in a flight so that an injection direction of the fuel is modified. |
| 地址 |
Tokyo JP |
