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.
申请公布号 US7363763(B2) 申请公布日期 2008.04.29
申请号 US20030691790 申请日期 2003.10.23
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;F23R3/42;F23R3/00 主分类号 F23R3/06
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