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US Patent 8256706 Integrated hypersonic inlet design

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Date Filed
October 8, 2009
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Date of Patent
September 4, 2012
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Patent Application Number
12575643
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Patent Citations Received
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US Patent 12122534 Direct design method for generating osculating curved wave-rider based on complex leading-edge profile
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US Patent 11661184 Surface stiffness optimization to improve morphing surface accuracy
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US Patent 11878809 Aircraft propulsion assembly comprising two adjacent engines, of which the outlet nozzles have a straight portion in the vicinity of a median plane of the propulsion assembly
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Patent Inventor Names
Kevin G. Bowcutt
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Thomas R. Smith
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
8256706
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Patent Primary Examiner
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Christopher P Ellis
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