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Patent Searching and Data


Title:
STATOR BLADE FOR AXIAL COMPRESSOR
Document Type and Number:
Japanese Patent JPH0925897
Kind Code:
A
Abstract:

To prevent loss caused by secondary flow and downsize the whole device by twisting a blade near the end wall surface so as to coincide with the direction of boundary layer flow generated near the end wall surface part of the blade.

One end of a stator blade 1 is fixed onto the end wall surface 3 formed at a part of a shroud. In this case, the stator blade 1 is twisted near the contact parts with the end wall surface 3 at one end and the end wall surface at the other end so as to coincide with the direction of boundary layer flow 4. As a result, the parts near the end wall surface contact parts of the blade 1 are twisted large with different twist angles from a twist angle at a center part opposed to main flow from the view of a plurality of longitudinal sections of the stator blade 1. The boundary layer flow 4 thereby flows along the blade profile, so that the development and growth of secondary flow are suppressed, and the increase of loss is prevented to attain high efficiency while realizing a compact device.


Inventors:
KOBAYASHI KAZUYA
Application Number:
JP17488495A
Publication Date:
January 28, 1997
Filing Date:
July 11, 1995
Export Citation:
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Assignee:
MITSUBISHI HEAVY IND LTD
International Classes:
F04D19/00; F01D5/14; F04D29/54; (IPC1-7): F04D29/54; F04D19/00
Attorney, Agent or Firm:
Akasaka Saka (1 person outside)