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发明名称
DISTRIBUTED COOLING FOR GAS TURBINE ENGINE COMBUSTOR
摘要
A combustor component of a gas turbine engine includes a refractory metal core (RMC) microcircuit for self-regulating a cooling flow.
申请公布号
US2013025287(A1)
申请公布日期
2013.01.31
申请号
US201113193686
申请日期
2011.07.29
申请人
CUNHA FRANK J.
发明人
CUNHA FRANK J.
分类号
F23R3/42;F02C7/12
主分类号
F23R3/42
代理机构
代理人
主权项
地址
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