ANGLED REVERSE CORE GAS TURBINE ENGINE WITH WIDENED NOZZLE

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20150240745A1
SERIAL NO

14265856

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A propulsion system for an aircraft includes a furcated nozzle that has at least a first duct that extends from a first propulsor to a first trailing end duct opening and a second duct that extends from a second propulsor to a second trailing end duct opening.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

International Classification(s)

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  • 2014 Application Filing Year
  • F02K Class
  • 434 Applications Filed
  • 356 Patents Issued To-Date
  • 82.03 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances2014201520162017201820192020202120220255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Chandler, Jesse M South Windsor, US 136 1014
Lord, Wesley K South Glastonbury, US 91 1458
Suciu, Gabriel L Glastonbury, US 580 8113

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Patent Citation Ranking

  • 2 Citation Count
  • F02K Class
  • 10 % this patent is cited more than
  • 10 Age
Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges10671822101 - 1011 - 2021 - 3031 - 4041 - 50051015202530354045505560657075

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