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US Patent 7926260 Flexible shaft for gas turbine engine

Patent 7926260 was granted and assigned to United Technologies on April, 2011 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributors
Is a
Patent
Patent
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Current Assignee
United Technologies
United Technologies
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Date Filed
February 23, 2010
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Date of Patent
April 19, 2011
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Patent Application Number
12710863
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Patent Citations Received
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US Patent 12123432 Low noise turbine for geared turbofan engine
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US Patent 12084978 Epicyclic gear train
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US Patent 12085025 Gas turbine engine compressor arrangement
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US Patent 12123356 Gas turbine engine with higher low spool torque-to-thrust ratio
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US Patent 11661906 Propulsion system arrangement for turbofan gas turbine engine
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US Patent 11661894 Geared turbine engine with relatively lightweight propulsor module
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US Patent 11680492 Epicyclic gear train
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US Patent 11698007 Flexible support structure for a geared architecture gas turbine engine
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US Patent 11713713 Gas turbine engine front center body architecture
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US Patent 11754000 High and low spool configuration for a gas turbine engine
•••
Patent Inventor Names
Alessio Pescosolido
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Michael E. McCune
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William G. Sheridan
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
7926260
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Patent Primary Examiner
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Louis Casaregola
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