Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section

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United States of America Patent

PATENT NO 9476355
APP PUB NO 20130224009A1
SERIAL NO

13408147

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A midframe portion (213) of a gas turbine engine (210) is presented, and includes a compressor section (212) configured to discharge an air flow (211) directed in a radial direction from an outlet of the compressor section (212). Additionally, the midframe portion (213) includes a manifold (214) to directly couple the air flow (211) from the compressor section (212) outlet to an inlet of a respective combustor head (218) of the midframe portion (213).

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Patent Owner(s)

Patent OwnerAddress
SIEMENS ENERGY INC4400 ALAFAYA TRAIL ORLANDO FL 32826

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Little, David A Chuluota, US 34 898
McQuiggan, Gerard Orlando, US 6 140
Wasdell, David L Winter Park, US 3 14

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