| 发明名称 |
SYSTEM FOR VIBRATION DAMPING OF A FUEL NOZZLE WITHIN A COMBUSTOR |
| 摘要 |
A system for vibration damping a fuel nozzle within a combustor includes a support plate, a fuel nozzle passage that extends through the support plate and a cylindrical damping insert that is coaxially aligned within the fuel nozzle passage and at least partially defines the fuel nozzle passage. The damping insert may include a metallic-mesh liner. |
| 申请公布号 |
US2014338343(A1) |
申请公布日期 |
2014.11.20 |
| 申请号 |
US201313893721 |
申请日期 |
2013.05.14 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
Ouellet Dereck Joseph;Huffman Marcus Byron;Overby Brandon Taylor;Tilley Stephen Wayne |
| 分类号 |
F23R3/28 |
主分类号 |
F23R3/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system for vibration damping a fuel nozzle within a combustor, comprising:
a. a support plate; b. a fuel nozzle passage that extends through the support plate; and c. a cylindrical damping insert coaxially aligned within the fuel nozzle passage, wherein the damping insert at least partially defines the fuel nozzle passage. |
| 地址 |
Schenectady NY US |
