Title:
MOVING BLADE OR STATOR BLADE FOR AXIAL-FLOW COMPRESSOR
Document Type and Number:
Japanese Patent JPS5999096
Kind Code:
A
Abstract:
A rotor or stator blade for an axial flow compressor has one or both of its end portions designed to minimize the interference between the annulus boundary layer and the blade. The basis of the invention is that the aerofoil is designed so that each section of the aerofoil through the boundary layer performs a constant amount of work per unit height.
Inventors:
KURISUTOFUAA FURIIMAN
Application Number:
JP19164083A
Publication Date:
June 07, 1984
Filing Date:
October 13, 1983
Export Citation:
Assignee:
ROLLS ROYCE
International Classes:
F04D29/38; F04D29/32; F04D29/54; (IPC1-7): F04D29/38; F04D29/54
Domestic Patent References:
| JP28006381A |
Attorney, Agent or Firm:
Kyozo Yuasa
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