Composite shroud and methods for attaching the shroud to plural blades
Provided are a method and impeller for a turbo-machine. The impeller includes a metallic base (1502) having a central hole, a back surface (1502b) and a front surface (1502a) opposite to the back surface (1502b); plural blades (1504, 1506) extending on the front surface (1502a) of the metallic base...
Saved in:
Main Authors | , , , , , |
---|---|
Format | Patent |
Language | Chinese English |
Published |
16.05.2012
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | Provided are a method and impeller for a turbo-machine. The impeller includes a metallic base (1502) having a central hole, a back surface (1502b) and a front surface (1502a) opposite to the back surface (1502b); plural blades (1504, 1506) extending on the front surface (1502a) of the metallic base (1502); a composite shroud (1508) attached to the plural blades (1504, 1506) such that plural closed paths or vanes are formed by the front surface (1502a) of the metallic base (1502), the plural blades (1504, 1506) and the composite shroud (1508); and connecting means (1510, 1606, 1706, 1806, 1906, 2302, 2410, 2608, 2612, 3002, 3010, 3402, 3510) configured to attach the composite shroud (1508) to the metallic base (1502) or the plural blades (1504, 1506). |
---|---|
Bibliography: | Application Number: CN2010830778 |