US Patent 10287991 Gas turbine engine with paired distributed fan sets
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A gas turbine engine comprises a gas generator rotating along a first axis of rotation, with at least one compressor rotor, at least one gas generator turbine rotor and a combustion section. A fan drive turbine rotates along a second axis of rotation, downstream of at least one gas generator turbine rotor. The fan drive turbine drives a pair of shaft portions extending in opposed directions beyond the axis of rotation of the gas generator.
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Patent Number
102879910
Date of Patent
May 14, 2019
0Patent Application Number
146001010
Date Filed
January 20, 2015
0Official Website
Patent Citations Received
Patent Primary Examiner
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Patent Jurisdiction
Patent Number
102879910
Date of Patent
May 14, 2019
0Patent Application Number
146001010
Date Filed
January 20, 2015
0Official Website
Patent Citations Received
Patent Primary Examiner
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US Patent 10287991 Gas turbine engine with paired distributed fan sets
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10287991
Date of patent
May 14, 2019
Patent application number
14600101
Date Filed
January 20, 2015
Patent primary examiner
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