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US Patent 10830144 Gas turbine engine compressor impeller cooling air sinks
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Edits on 9 Oct, 2024
"update inverses"
Golden AI
edited on 9 Oct, 2024
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Patent Citations Received
US Patent 12110820 Gas turbine engine centrifugal compressor with impeller load and cooling control
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Edits on 22 May, 2024
"update inverses"
Golden AI
edited on 22 May, 2024
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+1
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Patent Citations Received
US Patent 11988155 Combined power system
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Edits on 1 Feb, 2024
"update inverses"
Golden AI
edited on 1 Feb, 2024
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+1
properties)
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Patent Citations Received
US Patent 11885349 Compressor having a dual-impeller
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Edits on 4 Oct, 2023
"update inverses"
Golden AI
edited on 4 Oct, 2023
Edits made to:
Infobox
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+1
properties)
Infobox
Patent Citations Received
US Patent 11773773 Gas turbine engine centrifugal compressor with impeller load and cooling control
Edits on 7 Sep, 2023
"update inverses"
Golden AI
edited on 7 Sep, 2023
Edits made to:
Infobox
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+1
properties)
Infobox
Patent Citations Received
US Patent 11746695 Turbine engine with centrifugal compressor having impeller backplate offtake
Edits on 24 May, 2023
"Remove website redirecting to Patent Public Search front page"
Golden AI
edited on 24 May, 2023
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-1
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10830144
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Edits on 22 Apr, 2023
"update citations for inverse infoboxes"
Golden AI
edited on 22 Apr, 2023
Infobox
Patent Citations
US Patent 10415391 Rotor and gas turbine engine including a rotor
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Edits on 4 Apr, 2023
"Entity importer update"
Golden AI
edited on 4 Apr, 2023
Infobox
Is a
Patent
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
10830144
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Date of Patent
November 10, 2020
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Patent Application Number
15259883
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Date Filed
September 8, 2016
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10830144
0
Patent Citations
US Patent 10359051 Impeller shroud supports having mid-impeller bleed flow passages and gas turbine engines including the same
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US Patent 10415391 Rotor and gas turbine engine including a rotor
0
Patent Citations Received
US Patent 11525393 Turbine engine with centrifugal compressor having impeller backplate offtake
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Patent Primary Examiner
Gerald L Sung
0
Edits on 14 Dec, 2022
"update inverses"
Golden AI
edited on 14 Dec, 2022
Edits made to:
Infobox
(
+1
properties)
Infobox
Patent Citations Received
US Patent 11525393 Turbine engine with centrifugal compressor having impeller backplate offtake
0
Edits on 26 Sep, 2022
"Entity importer update"
Golden AI
edited on 26 Sep, 2022
Infobox
Is a
Patent
0
Patent Jurisdiction
United States Patent and Trademark Office
0
Patent Number
10830144
0
Date of Patent
November 10, 2020
0
Patent Application Number
15259883
0
Date Filed
September 8, 2016
0
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10830144
0
Patent Citations
US Patent 10359051 Impeller shroud supports having mid-impeller bleed flow passages and gas turbine engines including the same
0
US Patent 10415391 Rotor and gas turbine engine including a rotor
0
Patent Primary Examiner
Gerald L Sung
0
"update citations for inverse infoboxes"
Golden AI
edited on 26 Sep, 2022
Infobox
Patent Citations
US Patent 10359051 Impeller shroud supports having mid-impeller bleed flow passages and gas turbine engines including the same
0
Edits on 22 Sep, 2022
"update citations for inverse infoboxes"
Golden AI
edited on 22 Sep, 2022
Infobox
Patent Citations
US Patent 10415391 Rotor and gas turbine engine including a rotor
0
Edits on 17 Jun, 2022
"Entity importer update"
Golden AI
edited on 17 Jun, 2022
Edits made to:
Infobox
(
+1
properties)
Infobox
Website URL
https://pdfpiw.uspto.gov/.piw?Docid=10830144
Edits on 7 Feb, 2022
"Created via: Entity Importer"
Golden AI
created this topic on 7 Feb, 2022
Edits made to:
Infobox
(
+9
properties)
US Patent 10830144 Gas turbine engine compressor impeller cooling air sinks
Infobox
Is a
Patent
Patent jurisdiction
United States Patent and Trademark Office
Patent number
10830144
Date of patent
November 10, 2020
Patent application number
15259883
Date Filed
September 8, 2016
Patent citations
US Patent 10359051 Impeller shroud supports having mid-impeller bleed flow passages and gas turbine engines including the same
US Patent 10415391 Rotor and gas turbine engine including a rotor
Patent primary examiner
Gerald L Sung
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