发明名称 Combustor and gas turbine
摘要 A combustor of the present invention includes: a plurality of nozzles which is arranged around the central axis of a combustor and of which each base end is connected to an oil supply tube; a nozzle tube base which supports the plurality of nozzles and includes an oil chamber supplying fuel to the nozzles via an oil inflow portion provided in each oil supply tube; a first guide portion which faces the center of the combustor inside the oil chamber and guides the oil remaining inside the oil chamber to the oil inflow portion; and a second guide portion which faces the base end of the combustor inside the oil chamber and guides the oil remaining inside the oil chamber to the oil inflow portion.
申请公布号 US8695348(B2) 申请公布日期 2014.04.15
申请号 US20100913114 申请日期 2010.10.27
申请人 OMAE KATSUYOSHI;TANIGUCHI KENTA;TERADA YOSHITAKA;ONOZUKA TAKASHI;MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 OMAE KATSUYOSHI;TANIGUCHI KENTA;TERADA YOSHITAKA;ONOZUKA TAKASHI
分类号 F02C7/22 主分类号 F02C7/22
代理机构 代理人
主权项
地址