| 发明名称 | Combustion system and method of assembling the same | ||
| 摘要 | A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure. | ||
| 申请公布号 | US8893382(B2) | 申请公布日期 | 2014.11.25 |
| 申请号 | US201113249868 | 申请日期 | 2011.09.30 |
| 申请人 | General Electric Company | 发明人 | Patterson David Bruce;Corsmeier Donald Michael;Young Craig Douglas;Gardner Donald Lee;Thompson James Edward;Brown Daniel Dale;Wiehe Glenn Edward;Yeager Donald Scott;Marusko Mark Willard;Zerbe Michael Joseph |
| 分类号 | B23P17/00;F23R3/50;F23R3/00;F23R3/60 | 主分类号 | B23P17/00 |
| 代理机构 | Armstrong Teasdale LLP | 代理人 | Andes, Esq. William Scott;Armstrong Teasdale LLP |
| 主权项 | 1. A method of assembling a combustion system for a gas turbine engine, said method comprising: providing a combustion chamber frame, an inner casing structure, and an outer casing structure, wherein the combustion chamber frame includes a dome structure and a cowl integrally formed with the dome structure such that forward of the dome structure the cowl extends generally radially; and mounting the combustion chamber frame between the inner casing structure and the outer casing structure to at least partially define a forward boundary of a combustion chamber having a forward region and an aft region such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure closer to the forward region of the combustion chamber than the aft region of the combustion chamber. | ||
| 地址 | Schenectady NY US | ||