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公开(公告)号:US10082083B2
公开(公告)日:2018-09-25
申请号:US14978261
申请日:2015-12-22
Applicant: General Electric Company
Abstract: A drain system for a combustor of a gas turbine includes a plurality of drain tubes, a vertical header connected to an end of each drain tube to receive a fluid flow therefrom, and a horizontal header downstream of the vertical header and in fluid communication therewith. Each drain tube has another end adapted to be connected to a respective combustor can of the gas turbine to drain liquid therefrom. The vertical header is disposed at an angle between 30° and 90° with a horizontal plane.