Gas turbine engine rotor sections held together by tie shaft, and with blade rim undercut

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8459943
APP PUB NO 20110223025A1
SERIAL NO

12720771

Stats

ATTORNEY / AGENT: (SPONSORED)

Importance

Loading Importance Indicators... loading....

Abstract

See full text

An integrally bladed rotor is utilized in at least a stage of one of a compressor and turbine section. Airfoils extend radially outwardly from a platform, and there is an undercut inward from the platform at a downstream edge of the airfoil.

Loading the Abstract Image... loading....

First Claim

See full text

Family

Loading Family data... loading....

Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

International Classification(s)

  • [Classification Symbol]
  • [Patents Count]

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Barnes, Roland R Bloomfield, US 4 75
Benjamin, Daniel Simsbury, US 36 298
Schutte, Peter San Diego, US 1 10

Cited Art Landscape

Load Citation

Patent Citation Ranking

Forward Cite Landscape

Load Citation