US Patent 7350360 Annular combustor for a gas turbine
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Patent abstract
The invention relates to an annular combustor (13) for a gas turbine (10), into which combustor (13) burners (14, 15) open on an inlet side, and which combustor (13) extends in the axial direction from the inlet side to an outlet side (33) and is lined on the insides with cooled liner segments (16, 17) for protection from the hot gases.
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US Patent 07350360 Annular combustor for a gas turbine US Patent 7350360 Annular combustor for a gas turbine
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Patent Number
0735036000
Patent Number
735036000
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Official Website
Edits on 24 Apr, 2023
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Infobox
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Patent Jurisdiction
Patent Number
073503600
Date of Patent
April 1, 2008
0Patent Application Number
106254670
Date Filed
July 23, 2003
0Official Website
Patent Primary Examiner
Edits on 23 Sep, 2022
Golden AI
Infobox
Is a
Patent Jurisdiction
Patent Number
073503600
Date of Patent
April 1, 2008
0Patent Application Number
106254670
Date Filed
July 23, 2003
0Official Website
Patent Primary Examiner
Edits on 17 Jun, 2022
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US Patent 07350360 Annular combustor for a gas turbine
Infobox
Is a
Patent jurisdiction
Patent number
07350360
Date of patent
April 1, 2008
Patent application number
10625467
Date Filed
July 23, 2003
Patent primary examiner
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