Fuel nozzle with flexible support structures

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United States of America Patent

PATENT NO 10190774
APP PUB NO 20170003029A1
SERIAL NO

15107263

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Importance

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Abstract

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A fuel nozzle apparatus for a gas turbine engine includes: a fuel discharge element having a discharge orifice communicating with a fuel supply connection; a static supporting structure; and a cantilevered flexible support structure interconnecting the supporting structure and the fuel discharge element, the flexible support structure having a first end connected to the static supporting structure, and a second end connected to the fuel discharge element.

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Patent Owner(s)

  • GENERAL ELECTRIC COMPANY

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bellardi, Jason Joseph Cincinnati, US 29 88
Mook, Joshua Tyler Loveland, US 77 287
Tu, Ting-Yu West Chester, US 5 52

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