发明名称 Turbine nozzle sector
摘要 A turbine nozzle sector that includes an outer platform segment and an inner platform segment between which there extends one or more hollow vanes is disclosed. Each vane presents a trailing edge cavity for feeding with cooling air and communicating with a plurality of vents distributed along the trailing edge of the vane, these vents serving to exhaust a fraction of the cooling air. The cavity communicates with an air outlet hole situated level with the outer platform and enabling a fraction of the cooling air to be exhausted.
申请公布号 US8192145(B2) 申请公布日期 2012.06.05
申请号 US20080185304 申请日期 2008.08.04
申请人 BACHA JEAN-LUC;BAUMAS OLIVIER JEAN DANIEL;LANCIAUX LUCIE;LAVISON SOPHIE;SNECMA 发明人 BACHA JEAN-LUC;BAUMAS OLIVIER JEAN DANIEL;LANCIAUX LUCIE;LAVISON SOPHIE
分类号 F01D5/18 主分类号 F01D5/18
代理机构 代理人
主权项
地址