US Patent 10443540 Thrust reversal for turbofan gas turbine engine
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Patent abstract
A method of thrust reversal operation according to an example of the present disclosure includes, among other things, permitting an increase in engine power when at least one criterion is not met and a thrust reverser is deployed, and denying the increase in engine power when the at least one criterion is met. A system for thrust reversal is also disclosed.
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Patent Inventor Names
Juan A. Marcos0
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Patent Number
104435400
Date of Patent
October 15, 2019
0Patent Application Number
147075000
Date Filed
May 8, 2015
0Patent Primary Examiner
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US Patent 10443540 Thrust reversal for turbofan gas turbine engine
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10443540
Date of patent
October 15, 2019
Patent application number
14707500
Date Filed
May 8, 2015
Patent primary examiner
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