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Title:
支持体の水平接合面におけるタービンノズル保持装置
Document Type and Number:
Japanese Patent JP4439239
Kind Code:
B2
Abstract:
Nozzles for a turbine have dovetail-shaped bases for reception in corresponding dovetail-shaped grooves in the carrier halves of a turbine. The nozzles at each of the horizontal joint faces of each carrier half have notches formed along their bases including an abutment face. Key slots are formed in the horizontal joint faces and receive keys bearing against the abutment faces. The keys are peened or screwed into the carrier half at the horizontal joint faces. Radial loading pins engage the end nozzle bases to bias the end nozzles radially inwardly without interfering with the keys retaining the nozzles in the grooves.

Inventors:
Bernard Arthur Couture
David Orth Fitz
Ronald Wayne Colson
James david surreal
Application Number:
JP2003369785A
Publication Date:
March 24, 2010
Filing Date:
October 30, 2003
Export Citation:
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Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F01D9/02; F01D5/32; F01D9/00; F01D9/04; F01D25/24
Domestic Patent References:
JP6001799U
JP63235601A
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Nobukazu Ito



 
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