Title:
TIP SHROUDED BLADE
Document Type and Number:
Japanese Patent JP2013167246
Kind Code:
A
Abstract:
To reduce the misalignmnet of tip shrouds during the operation of a turbine system.
A tip shrouded blade includes an airfoil rotatable about an axial centerline. A tip shroud connected at a radially outer tip of the airfoil is also included, wherein the tip shroud includes at least one portion angled about a tangential axis defined by the radially outer tip of the airfoil.
Inventors:
GHATE VINEET NINAD
BOMMONAKATTE HARISH
PIERSALL MATTHEW ROBERT
BOMMONAKATTE HARISH
PIERSALL MATTHEW ROBERT
Application Number:
JP2013020009A
Publication Date:
August 29, 2013
Filing Date:
February 05, 2013
Export Citation:
Assignee:
GEN ELECTRIC
International Classes:
F01D5/22
Domestic Patent References:
| JP2005214205A | 2005-08-11 |
Foreign References:
| US5238366A | 1993-08-24 |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka