The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 21, 2020

Filed:

Apr. 11, 2016
Applicant:

Mitsubishi Hitachi Power Systems, Ltd., Nishi-ku, Yokohama, JP;

Inventors:

Yasuo Takahashi, Yokohama, JP;

Takanori Shibata, Yokohama, JP;

Yasunori Kimura, Yokohama, JP;

Chihiro Myoren, Yokohama, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 19/02 (2006.01); F04D 29/54 (2006.01); F04D 29/66 (2006.01); F02C 3/22 (2006.01); F02C 6/08 (2006.01); F02C 3/06 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F04D 19/02 (2013.01); F02C 3/04 (2013.01); F02C 3/06 (2013.01); F02C 3/22 (2013.01); F02C 6/08 (2013.01); F04D 29/54 (2013.01); F04D 29/66 (2013.01); F04D 29/661 (2013.01); F04D 29/542 (2013.01); F05D 2220/32 (2013.01); F05D 2220/3216 (2013.01); F05D 2220/72 (2013.01); F05D 2230/50 (2013.01); F05D 2230/80 (2013.01); F05D 2240/40 (2013.01); Y02E 20/16 (2013.01); Y10T 29/49238 (2015.01);
Abstract

In a gas turbine manufacturing method for manufacturing a derivative gas turbine having a different cycle from a reference gas turbine including a reference compressor, a compressor of the derivative gas turbine is designed to add at least one additional stage further on an upstream side than a last stage of the reference compressor and on a downstream side of a bleed slit of a bleed chamber of the reference compressor, the compressor of the derivative gas turbine is manufactured on the basis of the design, and the derivative gas turbine is manufactured. Consequently, it is possible to manufacture a gas turbine that can secure a surge margin of a compressor with respect to fluctuation in the composition of fuel.


Find Patent Forward Citations

Loading…