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US Patent 11306654 Gas turbine engine system wear reduction

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Edits on 28 Apr, 2023
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Infobox
Patent Citations
‌
US Patent 10781754 System and method for rotor bow mitigation
0
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Infobox
Is a
Patent
Patent
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
113066540
Date of Patent
April 19, 2022
0
Patent Application Number
166952900
Date Filed
November 26, 2019
0
Patent Citations
‌
US Patent 10040577 Modified start sequence of a gas turbine engine
0
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US Patent 10125636 Bowed rotor prevention system using waste heat
0
‌
US Patent 10125691 Bowed rotor start using a variable position starter valve
0
‌
US Patent 10174678 Bowed rotor start using direct temperature measurement
0
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US Patent 10208629 Piezo-electric motor for bowed rotor mitigation
0
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US Patent 10221774 Speed control during motoring of a gas turbine engine
0
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US Patent 10358936 Bowed rotor sensor system
0
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US Patent 10443507 Gas turbine engine bowed rotor avoidance system
0
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US Patent 10436064 Bowed rotor start response damping system
0
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US Patent 10539079 Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
0
‌
US Patent 10718231 Method and system for mitigating bowed rotor operation of gas turbine engine
0
‌
US Patent 10760498 System and method for removing rotor bow in a gas turbine engine using mechanical energy storage device
0
‌
US Patent 10781754 System and method for rotor bow mitigation
0
‌
US Patent 10801371 Bowed rotor prevention system
0
‌
US Patent 10823014 Turbine engine for reducing rotor bow and method thereof
0
‌
US Patent 11015659 Bowed rotor prevention system for turbomachinery
0
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US Patent 11073086 Apparatus, assemblies, and methods for mitigating thermal bow in the rotor of an engine at start-up
0
Patent Primary Examiner
‌
Katheryn A Malatek
0
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Edits on 23 Sep, 2022
"Entity importer update"
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edited on 23 Sep, 2022
Infobox
Is a
Patent
Patent
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
113066540
Date of Patent
April 19, 2022
0
Patent Application Number
166952900
Date Filed
November 26, 2019
0
Patent Citations
‌
US Patent 10040577 Modified start sequence of a gas turbine engine
0
‌
US Patent 10125636 Bowed rotor prevention system using waste heat
0
‌
US Patent 10125691 Bowed rotor start using a variable position starter valve
0
‌
US Patent 10174678 Bowed rotor start using direct temperature measurement
0
‌
US Patent 10208629 Piezo-electric motor for bowed rotor mitigation
0
‌
US Patent 10221774 Speed control during motoring of a gas turbine engine
0
‌
US Patent 10358936 Bowed rotor sensor system
0
‌
US Patent 10443507 Gas turbine engine bowed rotor avoidance system
0
‌
US Patent 10436064 Bowed rotor start response damping system
0
‌
US Patent 10539079 Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
0
‌
US Patent 10718231 Method and system for mitigating bowed rotor operation of gas turbine engine
0
‌
US Patent 10760498 System and method for removing rotor bow in a gas turbine engine using mechanical energy storage device
0
‌
US Patent 10781754 System and method for rotor bow mitigation
0
‌
US Patent 10801371 Bowed rotor prevention system
0
‌
US Patent 10823014 Turbine engine for reducing rotor bow and method thereof
0
‌
US Patent 11015659 Bowed rotor prevention system for turbomachinery
0
‌
US Patent 11073086 Apparatus, assemblies, and methods for mitigating thermal bow in the rotor of an engine at start-up
0
Patent Primary Examiner
‌
Katheryn A Malatek
0
Edits on 18 May, 2022
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created this topic on 18 May, 2022
Edits made to:
Infobox (+24 properties)
Article (+611 characters)
‌

 US Patent 11306654 Gas turbine engine system wear reduction

Article

An engine system for an aircraft includes a first gas turbine engine, a second gas turbine engine, and a control system. The control system is configured to operate the first gas turbine engine with an idle fuel burn schedule in a taxi mode of the aircraft and operate the second gas turbine engine with a sub-idle fuel burn schedule in the taxi mode of the aircraft. The sub-idle fuel burn schedule includes a reduction of the idle fuel burn schedule. A fuel flow of the first gas turbine engine and the second gas turbine engine is increased above the idle fuel burn schedule prior to takeoff of the aircraft.

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
11306654
Date of patent
April 19, 2022
Patent application number
16695290
Date Filed
November 26, 2019
Patent citations
‌
US Patent 10040577 Modified start sequence of a gas turbine engine
‌
US Patent 10125636 Bowed rotor prevention system using waste heat
‌
US Patent 10125691 Bowed rotor start using a variable position starter valve
‌
US Patent 10174678 Bowed rotor start using direct temperature measurement
‌
US Patent 10208629 Piezo-electric motor for bowed rotor mitigation
‌
US Patent 10221774 Speed control during motoring of a gas turbine engine
‌
US Patent 10358936 Bowed rotor sensor system
‌
US Patent 10443507 Gas turbine engine bowed rotor avoidance system
‌
US Patent 10436064 Bowed rotor start response damping system
‌
US Patent 10539079 Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
‌
US Patent 10718231 Method and system for mitigating bowed rotor operation of gas turbine engine
‌
US Patent 10760498 System and method for removing rotor bow in a gas turbine engine using mechanical energy storage device
‌
US Patent 10781754 System and method for rotor bow mitigation
‌
US Patent 10801371 Bowed rotor prevention system
‌
US Patent 10823014 Turbine engine for reducing rotor bow and method thereof
‌
US Patent 11015659 Bowed rotor prevention system for turbomachinery
‌
US Patent 11073086 Apparatus, assemblies, and methods for mitigating thermal bow in the rotor of an engine at start-up
Patent primary examiner
‌
Katheryn A Malatek

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