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US Patent 11365706 Turbine engine system utilizing an augmented combustion module

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Is a
Patent
Patent

Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11365706
Date of Patent
June 21, 2022
Patent Application Number
17128080
Date Filed
December 19, 2020
Patent Citations
‌
US Patent 10145291 Rotary engine and method of combusting fuel
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US Patent 10450952 Turbofan engine assembly with gearbox
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US Patent 10501200 Engine assembly for an auxiliary power unit
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US Patent 10570816 Engine coupling arrangement
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US Patent 10590842 Compound engine assembly with bleed air
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US Patent 10605111 Turbine generator with an internal rotor support shaft
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US Patent 10648368 Drive assembly for a gas turbine engine
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US Patent 10107195 Compound cycle engine
...
Patent Primary Examiner
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Stephanie Sebasco Cheng
CPC Code
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F02C 7/32
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F02K 3/06
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F02B 41/10
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F02B 2041/12
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F02B 61/04
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F02B 53/14
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B64D 2027/026

A turbine engine system utilizes one or more augmented combustion modules to produce an exhaust that is fed into the turbine portion of the engine and wherein power is produced by the augmented combustion module for use to drive the main shaft and/or for auxiliary purposes. An augmented combustion module is configured between the compressor and the turbine of the engine and receives compressed air from the compressor and ignites an air/fuel-mixture to turn a shaft that can be used to produce power. The shaft may be coupled with an electrical power generator, a pump, a hydraulic or pneumatic power generator and/or power conversion or transmission devices and/or coupled with the main shaft of the turbine engine. The power from a power generator may be stored in a battery, hydraulic accumulator or pneumatic accumulator and may be used to power auxiliary electrical, hydraulic or pneumatic devices.

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