发明名称 |
Combustor |
摘要 |
A gas turbine engine combustor has forward bulkhead extending between inboard and outboard walls and cooperating therewith to define a combustor interior volume or combustion chamber. 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 and a perimeter having leading and trailing edges and first and second lateral edges. A number of cooling passageways have inlets on the panel exterior surface and outlets on the panel interior surface. A rail protrudes from the exterior surface and is recessed from the leading edge along a majority of the leading edge
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申请公布号 |
US2005086940(A1) |
申请公布日期 |
2005.04.28 |
申请号 |
US20030691790 |
申请日期 |
2003.10.23 |
申请人 |
COUGHLAN JOSEPH D.III;PACHECO-TOUGAS MONICA;HOKE JAMES B.;GOETSCHIUS ALAN J. |
发明人 |
COUGHLAN JOSEPH D.III;PACHECO-TOUGAS MONICA;HOKE JAMES B.;GOETSCHIUS ALAN J. |
分类号 |
F23R3/06;F23R3/00;F23R3/42;(IPC1-7):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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