发明申请
US20130318976A1 TURBOMACHINE COMBUSTOR NOZZLE AND METHOD OF FORMING THE SAME 审中-公开
涡轮搅拌机喷嘴及其形成方法

TURBOMACHINE COMBUSTOR NOZZLE AND METHOD OF FORMING THE SAME
摘要:
A turbomachine combustor nozzle includes a first plate member having a first plurality of openings, and a second plate member having a second plurality of openings that are configured and disposed to be in alignment with the first plurality of openings. A plurality of nozzle members extends through corresponding ones of the first plurality of openings and the second plurality of openings. Each of the plurality of nozzle members includes a solid core.
信息查询
0/0