US Patent 8684303 Gas turbine engine compressor arrangement
Patent 8684303 was granted and assigned to United Technologies on April, 2014 by the United States Patent and Trademark Office.
All edits
Edits on 1 Dec, 2023
Golden AI
Edits made to:
Article (+179 characters)
Article
Patent abstract
A gas turbine engine includes a spool along an engine centerline axis which drives a gear train, said spool includes a low pressure compressor with four (4) stages.
Edits on 4 Oct, 2023
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Patent Citations Received
Edits on 25 Sep, 2023
Golden AI
Edits made to:
Infobox (+4 properties)
Infobox
Patent Inventor Names
Brian D. Merry0
Christopher M. Dye0
Gabriel L. Suciu0
Steven B. Johnson0
Edits on 22 Jul, 2023
Golden AI
Edits made to:
Infobox (-1 properties)
Infobox
Official Website
Edits on 14 Jun, 2023
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Patent Citations Received
Edits on 22 May, 2023
Golden AI
Edits made to:
Infobox (+1/-1 properties)
US Patent 08684303 Gas turbine engine compressor arrangement US Patent 8684303 Gas turbine engine compressor arrangement
Infobox
Patent Number
08684303
Patent Number
8684303
Edits on 19 Jun, 2022
Golden AI
Edits made to:
Infobox (+1 properties)
Infobox
Website URL
Edits on 22 Dec, 2021
Golden AI
Edits made to:
Infobox (+8 properties)
US Patent 08684303 Gas turbine engine compressor arrangement
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
08684303
Date of patent
April 1, 2014
Patent application number
13340940
Date Filed
December 30, 2011
Patent primary examiner
Find more entities like US Patent 8684303 Gas turbine engine compressor arrangement
Use the Golden Query Tool to find similar entities by any field in the Knowledge Graph, including industry, location, and more.
