| 发明名称 |
METHODS OF REINFORCING COMBUSTOR APERTURE AND RELATED COMBUSTOR |
| 摘要 |
Various embodiments include methods of reinforcing apertures in turbomachine combustors, and related combustors. In various particular embodiments, a method of reinforcing an existing turbomachine combustor aperture includes: broaching the existing aperture to modify an initial profile of the existing aperture and form a modified profile, where the modified profile protrudes radially outwardly from an outer surface of the turbomachine combustor; and welding a combustor ring along an inner surface of the modified profile, where the modified profile enhances bonding between the existing aperture and the combustor ring. |
| 申请公布号 |
US2015292740(A1) |
申请公布日期 |
2015.10.15 |
| 申请号 |
US201214124874 |
申请日期 |
2012.12.28 |
| 申请人 |
General Electric Company |
发明人 |
Radlicz Andrzej Jacek;Kaczorowski Kamil Bazyli;Karpinski Mariusz Grzegorz;Strzelec Damian |
| 分类号 |
F23R3/00;B23P6/00 |
主分类号 |
F23R3/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of reinforcing an existing turbomachine combustor aperture, the method comprising:
broaching the existing aperture in the turbomachine combustor to modify an initial profile of the existing aperture in the turbomachine combustor and form a modified profile, wherein the initial profile is substantially co-planar with an outer surface of the turbomachine combustor, and wherein the modified profile protrudes radially outwardly from the outer surface of the turbomachine combustor; and welding the existing aperture to a combustor ring, wherein the modified profile enhances bonding between the existing aperture and the combustor ring. |
| 地址 |
Schenectady NY US |
