Aviation fuel tank with rigid wall for crash energy absorption

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United States of America Patent

PATENT NO 9321539
SERIAL NO

14668701

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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Embodiments of the present invention relate generally to fuel tanks for aviation, and particularly to construction of rigid tank walls that have been found useful in absorbing energy of a magnitude expected during a crash. In some aspects, the rigid tank wall construction includes particular materials, such as a thermoplastic resin matrix. In some aspects, the rigid tank wall construction includes a particular arrangement of reinforcing fibers, such as a twill weave pattern.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AEROSYSTEMS78370 PLAISIR

International Classification(s)

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  • 2015 Application Filing Year
  • D03D Class
  • 219 Applications Filed
  • 163 Patents Issued To-Date
  • 74.43 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances20152016201720182019202020212022202320240255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Briand, Valérie Saint-Ouen-du-Tilleul, FR 1 7

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Patent Citation Ranking

  • 3 Citation Count
  • D03D Class
  • 33.71 % this patent is cited more than
  • 9 Age
Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges5910492101 - 1011 - 2021 - 3041 - 5005101520253035404550556065707580859095100105110

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11.5 Year Payment $7400.00 $3700.00 $1850.00 Oct 26, 2027