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US Patent 8181905 Aircraft engine nacelle with translating inlet cowl

Patent 8181905 was granted and assigned to Rohr, Inc. on May, 2012 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Current Assignee
Rohr, Inc.
Rohr, Inc.
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Date Filed
December 17, 2008
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Date of Patent
May 22, 2012
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Patent Application Number
12337209
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Patent Citations Received
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US Patent 12025055 Variable geometry inlet for turbopropeller inlet pressure recovery optimization
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US Patent 11661887 Variable geometry inlet system
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US Patent 11686272 Aircraft propulsion system with variable area inlet
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US Patent 11767124 Aircraft propulsion system with variable area inlet
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US Patent 11840985 Aircraft propulsion system with variable area inlet
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Patent Inventor Names
Keith Towers Brown
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Michael Patrick McDonough
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Scott Gilzean
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
8181905
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Patent Primary Examiner
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Benjamin P Lee
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