发明申请
US20110283707A1 System for Cooling Turbine Combustor Transition Piece 有权
冷却涡轮燃烧器过渡系统

System for Cooling Turbine Combustor Transition Piece
摘要:
An air cooling hood offset from an exterior of the transition piece to define an air cooling passage between the air cooling hood and the exterior of the transition piece, wherein the air cooling hood comprises a plurality of air outlets disposed along the exterior of the transition piece, and the plurality of air outlets is configured to expel an airflow from the air cooling passage away from the exterior of the transition piece.
公开/授权文献
信息查询
0/0