Multi-stage amplification vortex mixture for gas turbine engine combustor

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United States of America Patent

PATENT NO 9222674
APP PUB NO 20130019604A1
SERIAL NO

13188451

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Abstract

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A multi-stage vortex mixer for a combustor of a gas turbine engine includes a vortex amplifier stage in communication with a first stage amplifier, the vortex amplifier stage in communication with a dilution hole.

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Patent Owner(s)

Patent OwnerAddress
RAYTHEON TECHNOLOGIES CORPORATION870 WINTER STREET WALTHAM MA 02451

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Brogan, Torence P Manchester, US 6 139
Cunha, Frank J Avon, US 77 1565

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