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Title:
ターボ機械用翼
Document Type and Number:
Japanese Patent JP5420729
Kind Code:
B2
Abstract:
A blade of a turbomachine, especially of a steam turbine, is characterized in that the chord length (sm) in the middle region of the blade airfoil is shorter than the chord lengths (s0, S1) in the tip-side region or root-side region of the blade airfoil. As a result of this, a distribution of a Zweifel parameter over the longitudinal extent of the blade airfoil is achieved which minimizes the losses of a blade cascade of the blades.

Inventors:
Grime Ralph
Havaketian Zite
McBean Ivan
Monette Simon-Pierre
Application Number:
JP2012166361A
Publication Date:
February 19, 2014
Filing Date:
July 26, 2012
Export Citation:
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Assignee:
ALSTOM Technology Ltd
International Classes:
F01D9/02; F01D5/14
Domestic Patent References:
JP10331791A
JP9032501A
JP10103002A
JP2002213206A
JP2001132696A
JP8114199A
Foreign References:
EP0833060A2
Attorney, Agent or Firm:
Einzel Felix-Reinhard
Takuya Kuno



 
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