Invention Grant
US08668449B2 Turbine exhaust diffuser with region of reduced flow area and outer boundary gas flow
有权
涡轮排气扩散器具有减少流动面积和外界气体流量的区域
- Patent Title: Turbine exhaust diffuser with region of reduced flow area and outer boundary gas flow
- Patent Title (中): 涡轮排气扩散器具有减少流动面积和外界气体流量的区域
-
Application No.: US12944210Application Date: 2010-11-11
-
Publication No.: US08668449B2Publication Date: 2014-03-11
- Inventor: John Orosa
- Applicant: John Orosa
- Applicant Address: US FL Orlando
- Assignee: Siemens Energy, Inc.
- Current Assignee: Siemens Energy, Inc.
- Current Assignee Address: US FL Orlando
- Main IPC: F01D17/14
- IPC: F01D17/14
Abstract:
An exhaust diffuser system and method for a turbine engine. The outer boundary may include a region in which the outer boundary extends radially inwardly toward the hub structure and may direct at least a portion of an exhaust flow in the diffuser toward the hub structure. At least one gas jet is provided including a jet exit located on the outer boundary. The jet exit may discharge a flow of gas downstream substantially parallel to an inner surface of the outer boundary to direct a portion of the exhaust flow in the diffuser toward the outer boundary to effect a radially outward flow of at least a portion of the exhaust gas flow toward the outer boundary to balance an aerodynamic load between the outer and inner boundaries.
Public/Granted literature
- US20110056179A1 TURBINE EXHAUST DIFFUSER WITH REGION OF REDUCED FLOW AREA AND OUTER BOUNDARY GAS FLOW Public/Granted day:2011-03-10
Information query
