发明名称 Combustor liner for a gas turbine and the manufacturing method thereof
摘要 PURPOSE: A liner for a combustor of a gas turbine and a manufacturing method thereof are provided to for a combustor liner to be easily manufactured by welding a plurality of circular arc-shaped outer wall plates with joining pins. CONSTITUTION: A liner(100) for a combustor comprises a cylinder shaped inner wall and an outer wall(120). A plurality of guide pins(111) and joining pins(112) are radially protruded from an outer surface of the cylinder shaped inner wall. The joining pins are protruded more higher than the guide pins. A front section of the guide pins contacts with an inner surface of a circular plate board(121). The circular plate board is welded in between a pair of the joining pins.
申请公布号 KR20120059142(A) 申请公布日期 2012.06.08
申请号 KR20100120776 申请日期 2010.11.30
申请人 DOOSAN HEAVY INDUSTRIES & CONSTRUCTION CO., LTD. 发明人 KIM, HO KEUN;CHUN, JAE CHUL;AN, YUN HO;IM, JI HYUK;CHOE, JIN HOON;CHON, MU HWAN
分类号 F02C3/14;F02C7/00;F23R3/42 主分类号 F02C3/14
代理机构 代理人
主权项
地址
您可能感兴趣的专利