Aeroengine nacelle

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 7090165
APP PUB NO 20040238687A1
SERIAL NO

10697945

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A nacelle (55) for a gas turbine engine (10), the engine (10) comprising accessories (34) mounted to a fan casing (28) and a core engine (9), the nacelle (55) substantially surrounds the engine (10) and comprises an intake (12) and a thrust reverser unit (31). The thrust reverser unit (31) is formed by two generally C-shaped portions (31a, 31b). The thrust reverser unit (31) is openable to provide access to the accessories (34) and the core engine (9). The nacelle (55) further comprises a fan containment casing (33) that is integral with the intake (12).

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE PLCKINGS PLACE 90 YORK WAY LONDON N1 9FX

International Classification(s)

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  • 2003 Application Filing Year
  • B64B Class
  • 23 Applications Filed
  • 6 Patents Issued To-Date
  • 26.09 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances2003200420052006200720080255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Jones, Emlyn Derby, GB 4 354
Stretton, Richard G Loughborough, GB 67 970

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Patent Citation Ranking

  • 58 Citation Count
  • B64B Class
  • 83.33 % this patent is cited more than
  • 19 Age
Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges31111 - 1011 - 2021 - 3031 - 4000.20.40.60.811.21.41.61.822.22.42.62.833.2

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