US Patent 7870721 Gas turbine engine providing simulated boundary layer thickness increase
Patent 7870721 was granted and assigned to United Technologies on January, 2011 by the United States Patent and Trademark Office.
All edits
Edits on 4 Apr, 2024
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Patent Citations Received
Edits on 27 Nov, 2023
Golden AI
Edits made to:
Article (+397 characters)
Article
Patent abstract
A nacelle assembly for a gas turbine engine includes a fan cowl disposed about an axis, a core cowl within the fan cowl and a bleed passage having an inlet that receives a bleed airflow and an outlet that discharges the bleed airflow in an upstream direction from the outlet. The bleed airflow is selectively introduced near a boundary layer of an inlet lip section of the fan cowl.
Edits on 19 Jul, 2023
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Patent Citations Received
Edits on 14 Jun, 2023
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Patent Citations Received
Edits on 25 May, 2023
Golden AI
Edits made to:
Infobox (+1/-1 properties)
US Patent 07870721 Gas turbine engine providing simulated boundary layer thickness increase US Patent 7870721 Gas turbine engine providing simulated boundary layer thickness increase
Infobox
Patent Number
0787072100
Patent Number
787072100
Edits on 19 May, 2023
Golden AI
Edits made to:
Infobox (-1 properties)
Infobox
Official Website
Edits on 27 Apr, 2023
Golden AI
Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
078707210
Date of Patent
January 18, 2011
0Patent Application Number
115950400
Date Filed
November 10, 2006
0Official Website
Patent Primary Examiner
Edits on 25 Sep, 2022
Golden AI
Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
078707210
Date of Patent
January 18, 2011
0Patent Application Number
115950400
Date Filed
November 10, 2006
0Official Website
Patent Primary Examiner
Edits on 4 Jun, 2022
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Website URL
Edits on 6 Dec, 2021
Golden AI
Edits made to:
Infobox (+8 properties)
US Patent 07870721 Gas turbine engine providing simulated boundary layer thickness increase
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
07870721
Date of patent
January 18, 2011
Patent application number
11595040
Date Filed
November 10, 2006
Patent primary examiner
Find more entities like US Patent 7870721 Gas turbine engine providing simulated boundary layer thickness increase
Use the Golden Query Tool to find similar entities by any field in the Knowledge Graph, including industry, location, and more.
By using this site, you agree to our Terms of Service.