发明名称 |
COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE |
摘要 |
A combustor assembly for a gas turbine engine is provided. The combustor assembly generally includes an annular dome and a liner. The liner at least partially defines a combustion chamber and includes the forward end received within a slot defined by the annular dome. Additionally, a heat shield is provided. The heat shield includes an end also received within the slot defined by the annular dome. A mounting assembly attaches the forward end of the liner and the end of the heat shield to the annular dome, such that the forward end of the liner and the end of the heat shield are co-mounted within the slot defined by the annular dome. |
申请公布号 |
CA2940046(A1) |
申请公布日期 |
2017.03.02 |
申请号 |
CA20162940046 |
申请日期 |
2016.08.25 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
BLOOM, NICHOLAS JOHN;KIRTLEY, DANIEL;KAHN, ADAM ROBERT |
分类号 |
F23R3/50;F23R3/60 |
主分类号 |
F23R3/50 |
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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