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US Patent 12000339 Integral superstructure for load path optimization

Patent 12000339 was granted and assigned to General Electric on June, 2024 by the United States Patent and Trademark Office.

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Contents

Is a
Patent
Patent
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Patent attributes

Patent Applicant
General Electric
General Electric
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Current Assignee
General Electric
General Electric
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
120003390
Patent Inventor Names
Christopher Williams0
John Alan Manteiga0
Joshua Tyler Mook0
Date of Patent
June 4, 2024
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Patent Application Number
175263400
Date Filed
November 15, 2021
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Patent Citations
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US Patent 9915173 Bearing support for a hot section of a turboshaft engine, and an associated turboshaft engine
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US Patent 7777155 System and method for an integrated additive manufacturing cell for complex components
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US Patent 8469309 Monolithic structure for mounting aircraft engine
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US Patent 8506836 Methods for manufacturing components from articles formed by additive-manufacturing processes
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US Patent 8668442 Turbine nozzles and methods of manufacturing the same
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US Patent 11174786 Monolithic superstructure for load path optimization
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Patent Primary Examiner
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Gerald L Sung
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Patent abstract

The present disclosure generally relates to monolithic superstructures for supporting a rotating shaft coupled to a rotor relative to a stator. An integral superstructure supports the rotating component. The superstructure includes a bearing portion that contacts the shaft. A stator portion, is spaced a critical dimension radially outward, from the rotor. A first annular transfer portion extends axially forward from the bearing to the stator portion. A second annular transfer portion extends axially aft from the stator portion to a mounting flange. The mounting flange connects the superstructure to a frame. The superstructure maintains a critical dimension between the rotor and the stator as the temperature of the superstructure increases. The rotor may be a compressor impeller in a gas turbine engine and the stator may be an aero component that transfers air into a combustor.

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