发明名称 |
Combustor |
摘要 |
A gas turbine engine combustor (20) has forward bulkhead (36) extending between inboard and outboard walls (32, 34) and cooperating therewith to define a combustor interior volume or combustion chamber (30). At least one of the walls has an exterior shell and an interior shell including a number of panels. Each panel has interior and exterior surfaces (102, 104) and a perimeter having leading and trailing edges (106, 108) and first and second lateral edges (110, 112). A number of cooling passageways (140) have inlets on the panel exterior surface (104) and outlets on the panel interior surface (102). A rail (114) protrudes from the exterior surface and is recessed from the leading edge (106) along a majority of the leading edge (106). <IMAGE> |
申请公布号 |
EP1528322(A3) |
申请公布日期 |
2005.06.08 |
申请号 |
EP20040256079 |
申请日期 |
2004.10.01 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
COUGHLAN III, JOSEPH D.;PACHECO-TOUGAS, MONICA;HOKE, JAMES B.;GOETSCHIUS, ALAN J. |
分类号 |
F23R3/06;F23R3/00;F23R3/42 |
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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