Gas turbine engine with low stage count low pressure turbine and engine mounting arrangement

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 11286883
APP PUB NO 20200284222A1
SERIAL NO

16405149

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Importance

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Abstract

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A gas turbine engine includes, among other things, a fan section including a fan rotor, a gear train defined about an engine axis of rotation, a high spool, and a low spool including a low pressure turbine that drives the fan rotor through the gear train. A static structure includes a first engine mount location and a second engine mount location.

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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
Dye, Christopher M San Diego, US 119 2646
Johnson, Steven B Marlborough, US 44 661
Merry, Brian D Andover, US 210 3873
Schwarz, Frederick M Glastonbury, US 446 5139
Suciu, Gabriel L Glastonbury, US 580 8113

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