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US Patent 10718215 Airfoil with stepped spanwise thickness distribution
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Edits on 23 May, 2023
"Remove website redirecting to Patent Public Search front page"
Golden AI
edited on 23 May, 2023
Edits made to:
Infobox
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-1
properties)
Infobox
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10718215
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Edits on 23 Apr, 2023
"Entity importer update"
Golden AI
edited on 23 Apr, 2023
Infobox
Is a
Patent
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Patent Applicant
Pratt & Whitney Canada
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Current Assignee
Pratt & Whitney Canada
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
10718215
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Date of Patent
July 21, 2020
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Patent Application Number
15808060
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Date Filed
November 9, 2017
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10718215
0
Patent Citations
US Patent 10233758 Detuning trailing edge compound lean contour
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US Patent 10309236 Subsonic shock strut
0
US Patent 10280756 Gas turbine engine airfoil
0
Patent Primary Examiner
Woody A Lee, Jr.
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Edits on 28 Sep, 2022
"update citations for inverse infoboxes"
Golden AI
edited on 28 Sep, 2022
Infobox
Patent Citations
US Patent 10233758 Detuning trailing edge compound lean contour
0
Edits on 26 Sep, 2022
"update citations for inverse infoboxes"
Golden AI
edited on 26 Sep, 2022
Infobox
Patent Citations
US Patent 10309236 Subsonic shock strut
0
Edits on 8 Jun, 2022
"Entity importer update"
Golden AI
edited on 8 Jun, 2022
Edits made to:
Infobox
(
+1
properties)
Infobox
Website URL
https://pdfpiw.uspto.gov/.piw?Docid=10718215
Edits on 5 Feb, 2022
"Created via: Entity Importer"
Golden AI
created this topic on 5 Feb, 2022
Edits made to:
Infobox
(
+12
properties)
US Patent 10718215 Airfoil with stepped spanwise thickness distribution
Infobox
Is a
Patent
Patent applicant
Pratt & Whitney Canada
Current assignee
Pratt & Whitney Canada
Patent jurisdiction
United States Patent and Trademark Office
Patent number
10718215
Date of patent
July 21, 2020
Patent application number
15808060
Date Filed
November 9, 2017
Patent citations
US Patent 10233758 Detuning trailing edge compound lean contour
US Patent 10309236 Subsonic shock strut
US Patent 10280756 Gas turbine engine airfoil
Patent primary examiner
Woody A Lee, Jr.
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