专利名称：COMBUSTOR ASSEMBLY FOR A TURBINE
ENGINE
发明人：Nicholas John Bloom,Daniel Kirtley,Michael
Alan Stieg,Brian Christopher Towle,ChadHolden Sutton
申请号：US14842883申请日：20150902
公开号：US20170059160A1公开日：20170302
专利附图：
摘要：A combustor assembly for a gas turbine engine is provided. The combustor
assembly includes a liner at least partially defining a combustion chamber and extendingbetween an aft end a forward end generally along an axial direction. The combustorassembly also includes an annular dome including an enclosed surface defining a slot forreceipt of the forward end of the liner. A cap is positioned at the forward end of the linerand at least partially positioned within the slot defined by the enclosed surface of theannular dome. The cap includes a surface configured to contact at least one of theenclosed surface of the annular dome and the forward end of the liner. Such a
configuration may form a substantially airtight seal between the forward end of the linerand the annular dome despite a relative thermal expansion between the components.
申请人：General Electric Company
地址：Schenectady NY US
国籍：US
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