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Patent Searching and Data


Title:
GAS TURBINE COMBUSTOR
Document Type and Number:
WIPO Patent Application WO/2023/243734
Kind Code:
A1
Abstract:
This gas turbine combustor comprises: a shell that surrounds a combustion chamber; a liner that is positioned inward of the shell, and faces the combustion chamber; and a fitting that attaches the liner to the shell. The fitting includes: a support that includes a shaft portion running through the shell, and a head portion connected to the shaft portion and supporting the liner from the radially inner side of the shell; a fixing member that is attached to the shaft portion of the support on the radially outer side of the shell; a spacer that is interposed between the shell and the liner; and a biasing member that forms a gap between the spacer and the shell in the radial direction by biasing the liner radially inward such that the liner separates from the shell in the radial direction.

Inventors:
OZAKI YOSHIHIKO
MATSUYAMA RYUSUKE
Application Number:
PCT/JP2023/029157
Publication Date:
December 21, 2023
Filing Date:
August 09, 2023
Export Citation:
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Assignee:
KAWASAKI HEAVY IND LTD (JP)
International Classes:
F23R3/42; F02C7/20; F23R3/60
Foreign References:
US4944151A1990-07-31
JPH0338559U1991-04-15
JP2017002900A2017-01-05
JP2002506963A2002-03-05
JP2005509827A2005-04-14
US20160377296A12016-12-29
US20140109592A12014-04-24
US20160201910A12016-07-14
KR20190086266A2019-07-22
US5333443A1994-08-02
JPS6224016A1987-02-02
Attorney, Agent or Firm:
ARCO PATENT & TRADEMARK ATTORNEYS (JP)
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