| 发明名称 |
ULTRA COMPACT COMBUSTOR |
| 摘要 |
Embodiments of a combustor for a gas turbine engine are provided herein. In some embodiments, a combustion chamber for a gas turbine engine comprising may include a combustor having an inner volume defined at least partially by a front wall, wherein the wall comprises a plurality of facets each having a through hole fluidly coupled to the inner volume, and wherein the plurality of facets are oriented such that an axis of each of the plurality of facets is offset from a central axis of the combustor by an angle. |
| 申请公布号 |
US2015323184(A1) |
申请公布日期 |
2015.11.12 |
| 申请号 |
US201514706679 |
申请日期 |
2015.05.07 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
Tangirala Venkat Eswarlu;Joshi Narendra Digamber |
| 分类号 |
F23R3/00;F04D29/54;F23R3/44;F23R3/12;F23R3/34 |
主分类号 |
F23R3/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A combustion chamber for a gas turbine engine comprising:
a combustor having an inner volume defined at least partially by a front wall, wherein the wall comprises a plurality of facets each having a through hole fluidly coupled to the inner volume, and wherein the plurality of facets are oriented such that an axis of each of the plurality of facets is offset from a central axis of the combustor by an angle. |
| 地址 |
SCHENECTADY NY US |
