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US Patent 11686272 Aircraft propulsion system with variable area inlet

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Current Assignee
Rohr, Inc.
Rohr, Inc.
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Date Filed
September 10, 2021
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Date of Patent
June 27, 2023
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Patent Applicant
Rohr, Inc.
Rohr, Inc.
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Patent Application Number
17471933
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Patent Citations
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US Patent 10308368 Turbofan engine and method of reducing air flow separation therein
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US Patent 10221764 Variable geometry inlet system
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US Patent 7837142 Supersonic aircraft jet engine
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US Patent 8181905 Aircraft engine nacelle with translating inlet cowl
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US Patent 8690097 Variable-geometry rotating spiral cone engine inlet compression system and method
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US Patent 9908633 Variable-capture supersonic inlet
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US Patent 10107196 Adjustable size inlet system
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11686272
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Patent Primary Examiner
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Craig Kim
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CPC Code
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B64D 2033/0226
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B64D 2033/0286
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B64D 29/00
0
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B64D 29/06
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B64D 33/02
0
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F02C 7/04
0
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F02C 7/045
0
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F02K 1/12
0
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F02C 7/042
0
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B64D 2033/026
0

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