A gas turbine engine component is disclosed having a construction that permits a working fluid to flow from one side of the component to the other. In one embodiment the construction includes multiple layers, and in one particular embodiment the construction includes three layers. One or more layers can have different properties. Additionally, one or more layers of the construction can include a cellular structure. In one embodiment the component is a gas turbine engine combustor liner.
申请公布号
WO2011139314(A3)
申请公布日期
2014.04.03
申请号
WO2010US62382
申请日期
2010.12.29
申请人
ROLLS-ROYCE CORPORATION;BASTNAGEL, PHILIP, M.;RICE, EDWARD, CLAUDE