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:
Nov. 24, 2020

Filed:

May. 04, 2018
Applicant:

Doosan Heavy Industries & Construction Co., Ltd., Changwon-si, KR;

Inventor:

Kyung Kook Kim, Daejeon, KR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/28 (2006.01); F01D 25/24 (2006.01); F01D 25/26 (2006.01); F02C 7/28 (2006.01);
U.S. Cl.
CPC ...
F01D 25/285 (2013.01); F01D 25/243 (2013.01); F01D 25/246 (2013.01); F01D 25/265 (2013.01); F02C 7/28 (2013.01); F05D 2230/60 (2013.01); F05D 2230/64 (2013.01); F05D 2230/70 (2013.01); F05D 2240/55 (2013.01); F05D 2250/283 (2013.01);
Abstract

A method of assembling and disassembling a gas turbine, and a gas turbine assembled thereby, improves work efficiency and reduces time and cost by carrying out various disassembly and reassembly processes depending on circumstances. In one process, a turbine section is disassembled from a gas turbine by sequential steps of disassembling an upper turbine case; disassembling a rear diffuser assembly and a rear bearing assembly; disassembling a combustor assembly; disassembling a vane assembly; and disassembling a blade assembly. In another process, first-stage to fourth-stage blade assemblies and first-stage to fourth-stage vane assemblies in a turbine section are disassembled from the gas turbine by sequential steps of disassembling an upper turbine case; disassembling a combustor assembly; disassembling a vane assembly; and disassembling a blade assembly. The gas turbine includes a compressor section, a combustor section, and the turbine section assembled in a reverse order with respect to the disassembly method.


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