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US Patent 11433990 Active laminar flow control system with composite panel

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Date Filed
July 9, 2018
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Date of Patent
September 6, 2022
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Patent Applicant
Rohr, Inc.
Rohr, Inc.
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Patent Application Number
16030351
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Patent Citations
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US Patent 10005545 Aircraft wing rib
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US Patent 10377464 Method, injection moulding tool for manufacturing a leading edge section with hybrid laminar flow control for an aircraft, and leading edge section with hybrid laminar flow control obtained thereof
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US Patent 10414481 Method for forming a structural panel
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US Patent 10556670 Laminar flow panel
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US Patent 10532807 Leading edge with laminar flow control and manufacturing method thereof
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US Patent 10906659 Structured panel with structural reinforcement(s)
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US Patent 10676171 Structural panel with splice joint between adjacent core structures
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US Patent 10618636 Heat exchanger for laminar-flow aircraft
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US Patent 10000277 Perforated surface for suction-type laminar flow control
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Patent Citations Received
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US Patent 11959440 Acoustic attenuation structure made of composite material and method for manufacturing same
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Patent Inventor Names
Pablo T. Sanz Martinez
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Thomas Paolini
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Johann S. Schrell
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11433990
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Patent Primary Examiner
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Philip J Bonzell
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CPC Code
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B64C 2230/22
0
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B64D 29/00
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B64C 21/06
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B64C 1/12
0

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