发明名称 TURBOMACHINE FUEL-AIR MIXER COMPONENT INCLUDING AN ADDITIVELY MANUFACTURED PORTION JOINED TO A NON-ADDITIVELY MANUFACTURED PORTION AND METHOD
摘要 A turbomachine fuel-air mixer component includes a first component portion formed from a non-additive manufacturing process. The first component portion includes a plurality of tube elements each having an end portion. A second, additively manufactured component portion is additively joined to the first component portion. The second, additively manufactured component portion includes a plurality of additively manufactured tube sections constructed at, and fluidically connected with, respective ones of each end portion of the plurality of tube elements. The first and second component portions collectively defining at least a portion of the turbomachine fuel-air mixer component.
申请公布号 US2014361447(A1) 申请公布日期 2014.12.11
申请号 US201313911348 申请日期 2013.06.06
申请人 General Electric Company 发明人 Widener Stanley Kevin;Szabo Attila
分类号 F23R3/04 主分类号 F23R3/04
代理机构 代理人
主权项 1. A turbomachine fuel-air mixer component comprising: a first component portion formed from a non-additive manufacturing process, the first component portion including a plurality of tube elements each having an end portion including an end face; and a second, additively manufactured component portion additively joined to the first component portion, the second, additively manufactured component portion including a plurality of additively manufactured tube sections constructed at, and fluidically connected with, respective ones of each end portion of the plurality of tube elements, the first and second component portions collectively defining at least a portion of the turbomachine fuel-air mixer component.
地址 Schenectady NY US