Aerodynamic structure with asymmetrical shock bump

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United States of America Patent

PATENT NO 9896193
SERIAL NO

12735536

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An aerodynamic structure comprising a shock bump (3) extending from its surface. The shock bump is asymmetrical about a plane of asymmetry, and the plane of asymmetry: passes through a centre (6) of the shock bump, is parallel with a principal direction of air flow over the structure, and extends at a right angle to the surface of the structure.

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Patent Owner(s)

Patent OwnerAddress
AIRBUS OPERATIONS LIMITEDFILTON

International Classification(s)

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  • 2009 Application Filing Year
  • B64C Class
  • 646 Applications Filed
  • 484 Patents Issued To-Date
  • 74.93 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances200920102011201220132014201520162017201820190255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Wood, Norman Bristol, GB 18 112

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  • 0 Citation Count
  • B64C Class
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  • 7 Age
Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges85236227201 - 1011 - 2021 - 3031 - 40020406080100120140160180200220240260

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