US Patent 10550853 Gas turbine engine
Patent 10550853 was granted and assigned to Kawasaki on February, 2020 by the United States Patent and Trademark Office.
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Patent abstract
A gas turbine engine, in which a compressed gas from a compressor of an axial-flow type is burned in a combustor and an obtained combustion gas drives a turbine, includes: a diffuser of an annular shape connected to an outlet of the compressor, the diffuser including a diffuser inner tube and a diffuser outer tube that are tubular members disposed concentrically with each other; and a plurality of partition members that are disposed in a diffuser flow path, which is an annular space formed between the diffuser inner tube and the diffuser outer tube, and divide the diffuser flow path in a circumferential direction.
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Patent Inventor Names
Daisuke Uemura0
Hiroshi Kubo0
Koji Terauchi0
Naoto Sakai0
Toshimasa Miura0
Yuki Ishitobi0
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Infobox
Is a
Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
105508530
Date of Patent
February 4, 2020
0Patent Application Number
160130420
Date Filed
June 20, 2018
0Patent Citations Received
Patent Primary Examiner
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Patent Citations Received
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Patent citations received
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US Patent 10550853 Gas turbine engine
Infobox
Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
10550853
Date of patent
February 4, 2020
Patent application number
16013042
Date Filed
June 20, 2018
Patent primary examiner
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