Dual function cascade integrated variable area fan nozzle and thrust reverser

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 11499502
APP PUB NO 20200325849A1
SERIAL NO

16895037

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A gas turbine engine system according to an exemplary aspect of the present disclosure may include a core engine defined about an axis, a fan driven by the core engine about the axis to generate bypass flow, and at least one integrated mechanism in communication with the bypass flow. The at least one integrated mechanism includes a variable area fan nozzle (VAFN) and thrust reverser, and a plurality of positions to control bypass flow.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

International Classification(s)

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  • 2020 Application Filing Year
  • F02K Class
  • 367 Applications Filed
  • 247 Patents Issued To-Date
  • 67.31 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances2020202120222023202420250255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Marshall, Richard M Kirkland, CA 10 176

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Patent Citation Ranking

  • 1 Citation Count
  • F02K Class
  • 67.92 % this patent is cited more than
  • 3 Age
Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges1999401 - 100102030405060708090100110120130140150160170180190200210

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