发明名称 GAS TURBINE COMPONENT AND METHOD OF FORMING
摘要 Components (100) are disclosed which include a first component section (102) and a second component section (104) joined to form a hollow structure (106) defining a plenum (108) having an interior surface (110), wherein the component sections (102, 104) each include mating ridges (120, 122, 124, 126) joined together along the length (114) of the plenum (108), and a corrosion-resistant cladding layer (128) including a corrosion-resistant material (130) overlaying the interior surface (110) of the plenum (108). In one embodiment, the component (100) is a gas turbine combustor fuel manifold (604). A method of forming the components (100) includes applying corrosion-resistant segments (134, 136) including a corrosion-resistant material (130) to each of the surfaces (200, 300) of the component sections (102, 104), and joining the component sections (102, 104) to form the component (100), wherein joining the component sections (102, 104) includes fusing the corrosion-resistant segments (134, 136) into the corrosion-resistant cladding layer (128), and joining the mating ridges (120, 122, 124, 126) of the component sections (102, 104).
申请公布号 EP3144505(A1) 申请公布日期 2017.03.22
申请号 EP20160169761 申请日期 2016.05.16
申请人 General Electric Company 发明人 LIN, Dechao;KOTTILINGAM, Srikanth Chandrudu;DIAO, Xiaoxue;THOMAS, Nicholas
分类号 F02C7/22 主分类号 F02C7/22
代理机构 代理人
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