| 发明名称 |
COMBUSTOR, JET ENGINE, FLYING BODY, AND OPERATION METHOD OF JET ENGINE |
| 摘要 |
A combustor of a jet engine includes a fuel injector, an igniter for igniting a gas mixture of air and fuel, and a flame holder. The igniter is disposed in the flame holder. After an activation of the igniter, the igniter disappears, and a space after the disappearance functions as a flame-holding space. |
| 申请公布号 |
US2017030297(A1) |
申请公布日期 |
2017.02.02 |
| 申请号 |
US201515121172 |
申请日期 |
2015.02.13 |
| 申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
UENO Yoshihiko;YAMAMOTO Oto;SUZUKI Tasuku;FURUYA Shojiro |
| 分类号 |
F02K7/10;F02K9/78;F02K9/32 |
主分类号 |
F02K7/10 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A combustor in which fuel is burned using air taken through an inlet comprising:
an injector for injecting the fuel; a flame holder formed in a wall surface of the combustor and configured to keep flame for burning the fuel injected from the injector; and an igniter for igniting a gas mixture of the air and the fuel, wherein the igniter is disposed in the flame holder and configured to disappear to form a flame-holding space in the flame holder. |
| 地址 |
Tokyo JP |
