| 发明名称 |
Combustor |
| 摘要 |
<p>A gas turbine engine combustor (20) has inboard and outboard walls (32,134). A forward bulkhead (36) extends between the walls and cooperates therewith to define a combustor interior volume. In longitudinal section, a first portion (54) of the combustor interior volume converges from fore to aft and a second portion (56), aft of the first portion (54) converges from fore to aft more gradually than the first portion (54). <IMAGE></p> |
| 申请公布号 |
EP1522792(A1) |
申请公布日期 |
2005.04.13 |
| 申请号 |
EP20040256235 |
申请日期 |
2004.10.08 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BURD, STEVEN W.;CHEUNG, ALBERT K.;SEGALMAN, IRVING;OLS, JOHN T.;SMITH, REID D.C. |
| 分类号 |
F23R3/06;F23R3/00;F23R3/42;(IPC1-7):F23R3/00 |
主分类号 |
F23R3/06 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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