Invention Grant
US08727733B2 Gas turbine compressor last stage rotor blades with axial retention
有权
燃气轮机压缩机最后阶段转子叶片具有轴向保持力
- Patent Title: Gas turbine compressor last stage rotor blades with axial retention
- Patent Title (中): 燃气轮机压缩机最后阶段转子叶片具有轴向保持力
-
Application No.: US13116068Application Date: 2011-05-26
-
Publication No.: US08727733B2Publication Date: 2014-05-20
- Inventor: Anthony Constantine Thermos , Govindarajan Rengarajan , William John Miller , Max Robert Farson , Scott Yiming Yu
- Applicant: Anthony Constantine Thermos , Govindarajan Rengarajan , William John Miller , Max Robert Farson , Scott Yiming Yu
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Nixon & Vanderhye P.C.
- Main IPC: F01D5/32
- IPC: F01D5/32

Abstract:
A rotor blade and blade retention key assembly includes: a radially outer airfoil, a shank and a radially inner attachment dovetail. The attachment dovetail has a radially innermost surface formed with a notch at one axial end thereof, and a retention key is received in the notch, and rotatable from a retracted position where a retention key portion is substantially flush with the radially innermost surface, to an extended position where the retention key portion projects inwardly from said radially innermost surface and into a recess or pocket formed in a rotor wheel slot to prevent axial movement of the blade within the slot.
Public/Granted literature
- US20120301308A1 GAS TURBINE COMPRESSOR LAST STAGE ROTOR BLADES WITH AXIAL RETENTION Public/Granted day:2012-11-29
Information query