利索-全球专利检索

  1. 登录
  2. 注册
发明授权
US06331096B1 Apparatus and methods for impingement cooling of an undercut region adjacent a side wall of a turbine nozzle segment 有权
用于与涡轮喷嘴段的侧壁相邻的底切区域的冲击冷却的装置和方法

  • 专利标题： Apparatus and methods for impingement cooling of an undercut region adjacent a side wall of a turbine nozzle segment
  • 专利标题（中）： 用于与涡轮喷嘴段的侧壁相邻的底切区域的冲击冷却的装置和方法
  • 申请号： US09543457
    申请日： 2000-04-05
  • 公开(公告)号： US06331096B1
    公开(公告)日： 2001-12-18
  • 发明人: Steven Sebastian Burdgick , Gary Michael Itzel
  • 申请人： Steven Sebastian Burdgick , Gary Michael Itzel
  • 主分类号： F01D2508
  • IPC分类号： F01D2508
Apparatus and methods for impingement cooling of an undercut region adjacent a side wall of a turbine nozzle segment
摘要：
A gas turbine nozzle segment has outer and inner bands. Each band includes a side wall, a cover and an impingement plate between the cover and nozzle wall defining two cavities on opposite sides of the impingement plate. Cooling steam is supplied to one cavity for flow through apertures of the impingement plate to cool the nozzle wall. The side wall of the band and inturned flange define with the nozzle wall an undercut region. The inturned flange has a plurality of apertures for directing cooling steam to cool the side wall between adjacent nozzle segments.
摘要（中）：

燃气涡轮喷嘴段具有外带和内带。 每个带包括在盖和喷嘴壁之间的侧壁，盖和冲击板，其在冲击板的相对侧上限定两个空腔。 冷却蒸汽被供应到一个空腔以流过冲击板的孔以冷却喷嘴壁。 带和内壁凸缘的侧壁限定了喷嘴壁的底切区域。 内翻法兰具有多个孔，用于引导冷却蒸汽冷却相邻喷嘴段之间的侧壁。

信息查询
Espacenet
0/0