Title:
高効率発電方法、組立体、及びシステム
Document Type and Number:
Japanese Patent JP2013543550
Kind Code:
A
Abstract:
The present disclosure provides a turbine assembly, comprising a plurality of components including a casing defining an inlet configured to receive a combustion product stream, and an outlet, a rotor positioned in the casing, and a plurality of blades extending from the rotor, wherein a ratio of a length of the turbine assembly to an average diameter of the blades is greater than about 3.5, and wherein the length of the turbine assembly is a distance within the casing from the turbine blade immediately adjacent the inlet to the turbine blade immediately adjacent the outlet.
More Like This:
WO/2011/150979 | TRANSONIC GAS TURBINE STAGE AND METHOD |
WO/2014/025571 | ROTATING TURBINE COMPONENT WITH PREFERENTIAL HOLE ALIGNMENT |
JPH0719001 | TURBINE BLADE HAVING COOLING FLOW PASSAGE |
Inventors:
Palmer, Miles Earl.
Alam, Rodney John
Fettbet, Jeremy Elon
Alam, Rodney John
Fettbet, Jeremy Elon
Application Number:
JP2013529416A
Publication Date:
December 05, 2013
Filing Date:
September 20, 2011
Export Citation:
Assignee:
Palmer Lab, LRC
8 Rivers Capital, LRC
8 Rivers Capital, LRC
International Classes:
F01D5/18; B08B5/00; F01D5/28; F01D25/00; F01D25/12; F02C3/34; F02C6/18; F02C7/00; F02C7/052; F02C7/18; F23R3/00
Domestic Patent References:
JPS5519959A | 1980-02-13 | |||
JP2004257335A | 2004-09-16 | |||
JP2010065634A | 2010-03-25 | |||
JP2000511257A | 2000-08-29 | |||
JPH11303608A | 1999-11-02 | |||
JP2002129977A | 2002-05-09 |
Foreign References:
US6241469B1 | 2001-06-05 |
Attorney, Agent or Firm:
Ryoichi Takaoka
Nao Oda
Nao Oda