US Patent 10240529 Gas turbine engine aft bearing arrangement
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Patent abstract
An example gas turbine engine includes a turbine and first and second spools coaxial with one another. The first spool is arranged within the second spool and extends between forward and aft ends. The aft end extends axially beyond the second spool and supports the turbine. A housing is arranged downstream from the turbine. First and second bearings are mounted to the aft end of the first spool and supported by the housing portion.
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Patent Inventor Names
Gregory M. Savela0
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Patent Number
102405290
Date of Patent
March 26, 2019
0Patent Application Number
152744650
Date Filed
September 23, 2016
0Patent Primary Examiner
Edits on 25 Jan, 2022
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US Patent 10240529 Gas turbine engine aft bearing arrangement
Infobox
Is a
Patent jurisdiction
Patent number
10240529
Date of patent
March 26, 2019
Patent application number
15274465
Date Filed
September 23, 2016
Patent primary examiner
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