发明名称 COMBUSTION CHAMBER FOR A GAS TURBINE, AND TOOL AND METHOD FOR PRODUCING COOLING DUCTS IN A GAS TURBINE COMPONENT
摘要 A combustion chamber for a gas turbine has at least one housing component with a housing wall arranged around a hot-gas path and includes a hot side, which can be charged with hot gas, and an oppositely situated cold side. In the housing wall, there extends a number of cooling ducts each with an inner side, which cooling ducts each include an inflow region, which opens toward the cold side, and an outflow region, which opens into the interior of the combustion chamber. The combustion chamber permits cooling of the housing component, a reduction in pollutant emissions from the combustion chamber, and low production costs for the housing component. Turbulence generators are arranged in at least one of the cooling ducts, wherein the turbulence generators are web-like ribs which extend along the inner side of the cooling duct and which are formed integrally with the housing wall.
申请公布号 US2016199954(A1) 申请公布日期 2016.07.14
申请号 US201414914880 申请日期 2014.09.08
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 Hase Matthias
分类号 B23P19/04;F23R3/02 主分类号 B23P19/04
代理机构 代理人
主权项
地址 München DE