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US Patent 12017771 Slat-cove filler for wing structure of an aircraft

Overview Structured Data Issues Contributors Activity

Is a

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Patent attributes

Patent Jurisdiction

United States Patent and Trademark Office

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Patent Number

Patent Inventor Names

Mehdi R Khorrami0

Albert R. Allen0

Craig L. Streett0

Travis L Turner0

John W. Mulvaney0

Scott E Brynildsen0

David P Lockard0

Date of Patent

June 25, 2024

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Patent Application Number

172226040

Date Filed

April 5, 2021

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Patent Citations

US Patent 8469316 High-lift device, wing, and noise reduction structure for high-lift device

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US Patent 9242720 Autonomous slat-cove-filler device for reduction of aeroacoustic noise associated with aircraft systems

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US Patent 8695925 Elastically deformable side-edge link for trailing-edge flap aeroacoustic noise reduction

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US Patent 11427303 Noise abatement systems for retractable leading edge wing slats of an aircraft wing assembly

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US Patent 7766281 System for reducing aerodynamic noise at a supplementary wing of an aircraft

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US Patent 8424810 Low noise wing slat system with rigid cove-filled slat

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Patent Primary Examiner

Philip J Bonzell

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CPC Code

0

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Patent abstract

Methods, systems and devices of the various embodiments may provide slat-cove fillers configured to reduce leading-edge slat noise on aircraft, such as transport aircraft.

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