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2016
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Invention
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Epicyclic gear train. A turbine engine has a fan shaft. At least one tapered bearing is mounted o... |
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Invention
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Geared turbofan gas turbine engine architecture. A gas turbine engine typically includes a fan se... |
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Invention
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Advanced distributed engine architecture-design alternative. A gas turbine engine according to th... |
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Invention
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Geared turbofan engine with high compressor exit temperature. A gas turbine engine includes a fan... |
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Invention
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Geared turbofan engine with power density range. A gas turbine engine turbine has a high pressure... |
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2015
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Invention
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Low noise compressor rotor for geared turbofan engine. A gas turbine engine has a fan and a... |
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Invention
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Geared turbofan engine with low pressure environmental control system for aircraft. A gas turbine... |
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Invention
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Low noise compressor rotor for geared turbofan engine. A gas turbine engine comprises a fan and a... |
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2014
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Invention
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Geared gas turbine engine architecture for enhanced efficiency. An example gas turbine engine inc... |
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Invention
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Fundamental gear system architecture. A fan drive gear system for a gas turbine engine includes a... |
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Invention
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Geared architecture for high speed and small volume fan drive turbine. A gas turbine engine inclu... |
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Invention
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Elongated geared turbofan with high bypass ratio. A propulsion system includes a fan, a gear, a t... |
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Invention
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Method for setting a gear ratio of a fan drive gear system of a gas turbine engine. A gas turbine... |
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2013
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Invention
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Gas turbine engine with mount for low pressure turbine section. A gas turbine engine includes a v... |
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Invention
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Geared turbofan engine with increased bypass ratio and compressor ratio achieved with low stage a... |
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Invention
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Gas turbine engine with forward moment arm. A gas turbine engine includes a plurality of fan blad... |
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Invention
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Method for setting a gear ratio of a fan drive gear system of a gas turbine engine. A gas t... |
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Invention
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Pylon matched fan exit guide vane for noise reduction in a geared turbofan engine. A disclosed fa... |
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Invention
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Flexible support structure for a geared architecture gas turbine engine. A gas turbine engi... |
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Invention
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Fan drive gear system module and inlet guide vane coupling mechanism. A connection assembly for s... |
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Invention
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Geared fan with inner counter rotating compressor. A gas turbine engine comprises a fan section i... |
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Invention
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Manufacturing process for aerospace bearing rolling elements. A method of treating bearing rollin... |
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Invention
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Geared turbine engine with relatively lightweight propulsor module. An example gas turbine engine... |
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Invention
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Counter rotating low pressure compressor and turbine each having a gear system. A compressor sect... |
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Invention
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Counter-rotating low pressure turbine with gear system mounted to mid turbine frame. A gas turbin... |
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Invention
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Counter rotating low pressure turbine with splitter gear system. A gas turbine engine includes a ... |
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Invention
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Seal assembly for a static structure of a gas turbine engine. A static structure of a gas turbine... |
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Invention
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Geared turbofan gas turbine engine architecture. A gas turbine engine includes a fan rotatable ab... |
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Invention
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Gas turbine engine with high speed low pressure turbine section. A gas turbine engine includes a ... |
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Invention
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Gas turbine engine with high speed low pressure turbine section and bearing support features.
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Invention
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Low noise compressor rotor for geared turbofan engine. A gear reduction effects a reduction in th... |
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Invention
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Gas turbine engine with geared architecture. A gas turbine engine according to an exemplary aspec... |
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2012
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Invention
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Gas turbine engine with low stage count low pressure turbine. A gas turbine engine according to a... |
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Invention
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Gas turbine engine compressor arrangement. A gas turbine engine includes a fan section, a gear ar... |
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Invention
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Stator vane integrated attachment liner and spring damper. A stator subassembly includes an array... |
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Invention
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Stator vane spring damper. A stator subassembly includes an array of circumferentially arra... |
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Invention
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Gas turbine engine with low stage count low pressure turbine. A gas turbine engine includes a spo... |
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Invention
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Gas turbine engine compressor arrangement. A gas turbine engine includes a spool along an engine ... |
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Invention
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Dual function cascade integrated variable area fan nozzle and thrust reverser. A gas turbine engi... |
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Invention
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Gas turbine engine part retention. A gas turbine engine includes an engine casing structure and a... |
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Invention
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Gas turbine engine architecture with low pressure compressor hub between high and low rotor thrus... |
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Invention
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Hollow fan blade tuning using distinct filler materials. A fan blade comprises a main body extend... |
