Title:
ターボチャージャタービン及びコンプレッサのための輪郭付きブレード
Document Type and Number:
Japanese Patent JP2007511708
Kind Code:
A
Abstract:
A rotor and an apparatus including a rotor are provided. For example, the apparatus can be a turbine or compressor having a housing in which the rotor rotates while gas is circulated therethrough. The rotor has a plurality of radially extending blades, and each blade defines a nonlinear profile along at least one edge so that the strains induced in the blade during operation are reduced. A method for manufacturing such a rotor is also provided.
Inventors:
Jizawi, Nidal A
Application Number:
JP2006541387A
Publication Date:
May 10, 2007
Filing Date:
November 18, 2004
Export Citation:
Assignee:
Honeywell International Inc.
International Classes:
F01D5/14; F01D5/02; F02B39/00
Domestic Patent References:
JPH05340265A | 1993-12-21 | |||
JP2002364302A | 2002-12-18 | |||
JPH11190201A | 1999-07-13 |
Attorney, Agent or Firm:
Kazuo Shamoto
Shinjiro Ono
Yasushi Kobayashi
Akio Chiba
Hiroyuki Tomita
Fujihiro Kanda
Shinjiro Ono
Yasushi Kobayashi
Akio Chiba
Hiroyuki Tomita
Fujihiro Kanda