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US Patent 10760530 Fan arrangement for a gas turbine engine

Patent 10760530 was granted and assigned to Rolls-Royce on September, 2020 by the United States Patent and Trademark Office.

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Edits on 24 Jul, 2024
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edited on 24 Jul, 2024
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edited on 22 May, 2024
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Patent Citations Received
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US Patent 11988169 Fan arrangement for a gas turbine engine
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edited on 31 May, 2023
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Patent Citations Received
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US Patent 11661894 Geared turbine engine with relatively lightweight propulsor module
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Edits on 20 May, 2023
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edited on 20 May, 2023
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=1076053000
Edits on 26 Apr, 2023
"Entity importer update"
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edited on 26 Apr, 2023
Infobox
Is a
Patent
Patent
0
Patent Applicant
Rolls-Royce
Rolls-Royce
0
Current Assignee
Rolls-Royce
Rolls-Royce
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
107605300
Date of Patent
September 1, 2020
0
Patent Application Number
164235410
Date Filed
May 28, 2019
0
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=107605300
Patent Citations
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US Patent 10001083 Turbofan aircraft engine
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US Patent 10047699 Thrust efficient turbofan engine
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US Patent 10047700 Thrust efficient turbofan engine
0
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US Patent 10047701 Thrust efficient turbofan engine
0
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US Patent 10047702 Thrust efficient turbofan engine
0
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US Patent 10060357 Turbine section of high bypass turbofan
0
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US Patent 10060391 Thrust efficient turbofan engine
0
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US Patent 10179653 Pylon shape with geared turbofan for structural stiffness
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US Patent 10294894 Thrust efficient turbofan engine
0
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US Patent 10371061 Turbine section of high bypass turbofan
0
Patent Citations Received
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US Patent 11053947 Turbine engine
0
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US Patent 11339713 Large-scale bypass fan configuration for turbine engine core and bypass flows
0
Patent Primary Examiner
‌
Alain Chau
0
Edits on 23 Apr, 2023
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edited on 23 Apr, 2023
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edited on 3 Apr, 2023
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edited on 30 Mar, 2023
Edits on 26 Mar, 2023
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edited on 26 Mar, 2023
Edits on 26 Mar, 2023
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edited on 26 Mar, 2023
Edits on 22 Mar, 2023
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edited on 22 Mar, 2023
Edits on 28 Sep, 2022
"update citations for inverse infoboxes"
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edited on 28 Sep, 2022
Edits on 26 Sep, 2022
"update citations for inverse infoboxes"
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Golden AI
edited on 26 Sep, 2022
Infobox
Patent Citations Received
‌
US Patent 11053947 Turbine engine
0
"update citations for inverse infoboxes"
Golden AI profile picture
Golden AI
edited on 26 Sep, 2022
"update citations for inverse infoboxes"
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Golden AI
edited on 26 Sep, 2022
Edits on 26 Sep, 2022
"Entity importer update"
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Golden AI
edited on 26 Sep, 2022
Infobox
Is a
Patent
Patent
0
Patent Applicant
Rolls-Royce
Rolls-Royce
0
Current Assignee
Rolls-Royce
Rolls-Royce
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
107605300
Date of Patent
September 1, 2020
0
Patent Application Number
164235410
Date Filed
May 28, 2019
0
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=107605300
Patent Citations
‌
US Patent 10001083 Turbofan aircraft engine
0
‌
US Patent 10047699 Thrust efficient turbofan engine
0
‌
US Patent 10047700 Thrust efficient turbofan engine
0
‌
US Patent 10047701 Thrust efficient turbofan engine
0
‌
US Patent 10047702 Thrust efficient turbofan engine
0
‌
US Patent 10060357 Turbine section of high bypass turbofan
0
‌
US Patent 10060391 Thrust efficient turbofan engine
0
‌
US Patent 10179653 Pylon shape with geared turbofan for structural stiffness
0
‌
US Patent 10294894 Thrust efficient turbofan engine
0
‌
US Patent 10371061 Turbine section of high bypass turbofan
0
Patent Citations Received
‌
US Patent 11053947 Turbine engine
0
‌
US Patent 11339713 Large-scale bypass fan configuration for turbine engine core and bypass flows
0
Patent Primary Examiner
‌
Alain Chau
0
"update citations for inverse infoboxes"
Golden AI profile picture
Golden AI
edited on 25 Sep, 2022
Edits on 23 Sep, 2022
"update citations for inverse infoboxes"
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Golden AI
edited on 23 Sep, 2022
Edits on 22 Sep, 2022
"update citations for inverse infoboxes"
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Golden AI
edited on 22 Sep, 2022

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