Rotor blade for a gas turbine engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 10808539
APP PUB NO 20180023396A1
SERIAL NO

15218376

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Abstract

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A rotor blade for a gas turbine engine includes a blade extending from a root and a contoured tip portion at a first end of the blade. The first end is opposite the root. The contoured tip portion includes a first sloped region and a second sloped region. The second sloped region is steeper than the first sloped region, relative to a platform.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bintz, Matthew E West Hartford, US 48 293
Brilliant, Lisa I Middletown, US 42 182
Dong, Yuan Glastonbury, US 31 359
Monahan, Daniel J Cromwell, US 3 34
Murphy, Andrew J Old Saybrook, US 509 7038
Narrow, Taryn Glastonbury, US 5 19
Roberts, Steven D Moodus, US 18 290
Sorensen, Lucas D Middletown, US 1 9
Wall, Jordan T Middletown, US 7 24

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