US Patent 10508598 Cooling systems for gas turbine engines
All edits
Edits on 30 Oct, 2024
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Patent Citations Received
Edits on 9 Dec, 2023
Golden AI
Edits made to:
Article (+357 characters)
Article
Patent abstract
An air-oil cooler for a gas turbine engine includes an air cooling structure and a lubricant channel. The lubricant channel extends between a lubricant inlet and a lubricant inlet and is bounded by the air cooling structure. The air cooling structure has an arcuate shape for circumferentially spanning a portion of a gas turbine engine core.
Edits on 3 Oct, 2023
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Patent Inventor Names
Richard Alan Weiner0
Edits on 25 Apr, 2023
Golden AI
Infobox
Patent Citations
Edits on 5 Apr, 2023
Golden AI
Infobox
Patent Citations Received
Edits on 24 Mar, 2023
Golden AI
Infobox
Patent Citations
Edits on 1 Mar, 2023
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Patent Citations Received
Edits on 11 Jan, 2023
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Patent Citations Received
Edits on 25 Sep, 2022
Golden AI
Infobox
Patent Citations
Golden AI
Infobox
Patent Citations
Edits on 31 Jan, 2022
Golden AI
Edits made to:
Infobox (+12 properties)
US Patent 10508598 Cooling systems for gas turbine engines
Infobox
Is a
Patent jurisdiction
Patent number
10508598
Date of patent
December 17, 2019
Patent application number
15111997
Date Filed
December 22, 2014
Patent citations
Patent primary examiner
Find more entities like US Patent 10508598 Cooling systems for gas turbine engines
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.