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US Patent 11988140 Gas turbine engine inlet wall design

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Date Filed
January 12, 2021
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Date of Patent
May 21, 2024
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Patent Applicant
Raytheon Technologies
Raytheon Technologies
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Patent Application Number
17147129
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Patent Citations
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US Patent 8210474 Multi-path inlet for aircraft engine
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US Patent 8366050 Blended wing body cargo airplane
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US Patent 8302908 Blended wing aircraft
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US Patent 7644888 High-speed aircraft and methods for their manufacture
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US Patent 7665689 Unconventional integrated propulsion systems and methods for blended wing body aircraft
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US Patent 7861968 Air inlet and method for a highspeed mobile platform
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US Patent 8056852 Longitudinal flying wing aircraft
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Patent Inventor Names
Dmytro Mykolayovych Voytovych
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Om P. Sharma
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11988140
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Patent Primary Examiner
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Nicholas McFall
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CPC Code
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F02C 7/04
0
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F02K 3/12
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B64C 2039/105
0
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B64D 33/02
0

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