Invention Grant
- Patent Title: Cooling arrangement for a turbine component
- Patent Title (中): 涡轮机组件的冷却装置
-
Application No.: US12852688Application Date: 2010-08-09
-
Publication No.: US08647053B2Publication Date: 2014-02-11
- Inventor: Johan Hsu , Jay A. Morrison
- Applicant: Johan Hsu , Jay A. Morrison
- Applicant Address: US FL Orlando
- Assignee: Siemens Energy, Inc.
- Current Assignee: Siemens Energy, Inc.
- Current Assignee Address: US FL Orlando
- Main IPC: F01D25/12
- IPC: F01D25/12

Abstract:
A cooled component wall (52) with a combustion gas (36) on one side (56) and a coolant gas (48) with higher pressure on the other side (58). The wall includes a cooling chamber (60) with an impingement cooling zone (62), a convective cooling zone (64), and a film cooling zone (66). Impingement holes (70) admit and direct jets (72) of coolant against the wall, then the coolant passes among heat transfer elements such as channels (76) and fins (78) to the film cooling zone (66) where it passes through holes in the wall that direct a film of the coolant along the combustion side of the wall. The chamber may be oriented with the impingement zone (62) downstream and the film cooling zone (66) upstream, relative to the combustion gas flow (36). This provides two passes of the coolant (84, 79) in opposite directions over the respective opposite sides of the wall (56, 58).
Public/Granted literature
- US20120034075A1 COOLING ARRANGEMENT FOR A TURBINE COMPONENT Public/Granted day:2012-02-09
Information query