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US Patent 10876429 Shroud segment assembly intersegment end gaps control
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All edits
Edits on 19 May, 2023
"Remove website redirecting to Patent Public Search front page"
Golden AI
edited on 19 May, 2023
Edits made to:
Infobox
(
-1
properties)
Infobox
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10876429
0
0
Edits on 29 Apr, 2023
"update citations for inverse infoboxes"
Golden AI
edited on 29 Apr, 2023
Infobox
Patent Citations
US Patent 10443451 Shroud housing supported by vane segments
0
"update citations for inverse infoboxes"
Golden AI
edited on 29 Apr, 2023
Infobox
Patent Citations
US Patent 10077663 Gas turbine engine rotor stack assembly
0
Edits on 25 Apr, 2023
"update citations for inverse infoboxes"
Golden AI
edited on 25 Apr, 2023
Infobox
Patent Citations
US Patent 10550702 Turbine disk
0
Edits on 25 Apr, 2023
"update citations for inverse infoboxes"
Golden AI
edited on 25 Apr, 2023
Infobox
Patent Citations
US Patent 10280766 Bladed rotor for a gas turbine engine
0
"update citations for inverse infoboxes"
Golden AI
edited on 25 Apr, 2023
Infobox
Patent Citations
US Patent 10329929 Retaining ring axially loaded against segmented disc surface
0
Edits on 24 Apr, 2023
"update citations for inverse infoboxes"
Golden AI
edited on 24 Apr, 2023
Infobox
Patent Citations
US Patent 10400603 Mini-disk for gas turbine engine
0
Edits on 2 Apr, 2023
"Entity importer update"
Golden AI
edited on 2 Apr, 2023
Infobox
Is a
Patent
0
Patent Jurisdiction
United States Patent and Trademark Office
0
Patent Number
10876429
0
Date of Patent
December 29, 2020
0
Patent Application Number
16360489
0
Date Filed
March 21, 2019
0
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10876429
0
Patent Citations
US Patent 10077663 Gas turbine engine rotor stack assembly
0
US Patent 10221761 Turbine minidisk bumper for gas turbine engine
0
US Patent 10253642 Gas turbine engine with disk having periphery with protrusions
0
US Patent 10280766 Bladed rotor for a gas turbine engine
0
US Patent 10329929 Retaining ring axially loaded against segmented disc surface
0
US Patent 10370971 Reinforced gas turbine engine rotor disk
0
US Patent 10400603 Mini-disk for gas turbine engine
0
US Patent 10443451 Shroud housing supported by vane segments
0
US Patent 10550702 Turbine disk
0
Patent Citations Received
US Patent 11359505 Nesting CMC components
0
Patent Primary Examiner
Nathaniel E Wiehe
0
Edits on 23 Mar, 2023
"update citations for inverse infoboxes"
Golden AI
edited on 23 Mar, 2023
Infobox
Patent Citations
US Patent 10253642 Gas turbine engine with disk having periphery with protrusions
0
Edits on 27 Sep, 2022
"update citations for inverse infoboxes"
Golden AI
edited on 27 Sep, 2022
Infobox
Patent Citations
US Patent 10253642 Gas turbine engine with disk having periphery with protrusions
0
Edits on 26 Sep, 2022
"update citations for inverse infoboxes"
Golden AI
edited on 26 Sep, 2022
Infobox
Patent Citations
US Patent 10280766 Bladed rotor for a gas turbine engine
0
Edits on 25 Sep, 2022
"update citations for inverse infoboxes"
Golden AI
edited on 25 Sep, 2022
Infobox
Patent Citations
US Patent 10329929 Retaining ring axially loaded against segmented disc surface
0
"update citations for inverse infoboxes"
Golden AI
edited on 25 Sep, 2022
Infobox
Patent Citations
US Patent 10221761 Turbine minidisk bumper for gas turbine engine
0
"Entity importer update"
Golden AI
edited on 24 Sep, 2022
Infobox
Is a
Patent
0
Patent Jurisdiction
United States Patent and Trademark Office
0
Patent Number
10876429
0
Date of Patent
December 29, 2020
0
Patent Application Number
16360489
0
Date Filed
March 21, 2019
0
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10876429
0
Patent Citations
US Patent 10077663 Gas turbine engine rotor stack assembly
0
US Patent 10221761 Turbine minidisk bumper for gas turbine engine
0
US Patent 10253642 Gas turbine engine with disk having periphery with protrusions
0
US Patent 10280766 Bladed rotor for a gas turbine engine
0
US Patent 10329929 Retaining ring axially loaded against segmented disc surface
0
US Patent 10370971 Reinforced gas turbine engine rotor disk
0
US Patent 10400603 Mini-disk for gas turbine engine
0
US Patent 10443451 Shroud housing supported by vane segments
0
US Patent 10550702 Turbine disk
0
Patent Citations Received
US Patent 11359505 Nesting CMC components
0
Patent Primary Examiner
Nathaniel E Wiehe
0
Edits on 24 Sep, 2022
"update citations for inverse infoboxes"
Golden AI
edited on 24 Sep, 2022
Infobox
Patent Citations
US Patent 10550702 Turbine disk
0
Edits on 22 Sep, 2022
"update citations for inverse infoboxes"
Golden AI
edited on 22 Sep, 2022
Infobox
Patent Citations
US Patent 10077663 Gas turbine engine rotor stack assembly
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=10876429
Edits on 15 Jun, 2022
"update inverses"
Golden AI
edited on 15 Jun, 2022
Edits made to:
Infobox
(
+1
properties)
Infobox
Patent citations received
US Patent 11359505 Nesting CMC components
Edits on 8 Feb, 2022
"Created via: Entity Importer"
Golden AI
created this topic on 8 Feb, 2022
Edits made to:
Infobox
(
+16
properties)
US Patent 10876429 Shroud segment assembly intersegment end gaps control
Infobox
Is a
Patent
Patent jurisdiction
United States Patent and Trademark Office
Patent number
10876429
Date of patent
December 29, 2020
Patent application number
16360489
Date Filed
March 21, 2019
Patent citations
US Patent 10077663 Gas turbine engine rotor stack assembly
US Patent 10221761 Turbine minidisk bumper for gas turbine engine
US Patent 10253642 Gas turbine engine with disk having periphery with protrusions
US Patent 10280766 Bladed rotor for a gas turbine engine
US Patent 10329929 Retaining ring axially loaded against segmented disc surface
US Patent 10370971 Reinforced gas turbine engine rotor disk
US Patent 10400603 Mini-disk for gas turbine engine
US Patent 10443451 Shroud housing supported by vane segments
US Patent 10550702 Turbine disk
Patent primary examiner
Nathaniel E Wiehe
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