JP2014115072A5 - - Google Patents

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Publication number
JP2014115072A5
JP2014115072A5 JP2013206019A JP2013206019A JP2014115072A5 JP 2014115072 A5 JP2014115072 A5 JP 2014115072A5 JP 2013206019 A JP2013206019 A JP 2013206019A JP 2013206019 A JP2013206019 A JP 2013206019A JP 2014115072 A5 JP2014115072 A5 JP 2014115072A5
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JP
Japan
Prior art keywords
fuel
extending
distribution manifold
axially
upstream end
Prior art date
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Granted
Application number
JP2013206019A
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English (en)
Japanese (ja)
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JP2014115072A (ja
JP6266290B2 (ja
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Publication date
Priority claimed from US13/705,443 external-priority patent/US9291103B2/en
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Publication of JP2014115072A publication Critical patent/JP2014115072A/ja
Publication of JP2014115072A5 publication Critical patent/JP2014115072A5/ja
Application granted granted Critical
Publication of JP6266290B2 publication Critical patent/JP6266290B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013206019A 2012-12-05 2013-10-01 ガス・タービン・エンジンの燃焼器用燃料ノズル Active JP6266290B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/705,443 2012-12-05
US13/705,443 US9291103B2 (en) 2012-12-05 2012-12-05 Fuel nozzle for a combustor of a gas turbine engine

Publications (3)

Publication Number Publication Date
JP2014115072A JP2014115072A (ja) 2014-06-26
JP2014115072A5 true JP2014115072A5 (enExample) 2016-11-17
JP6266290B2 JP6266290B2 (ja) 2018-01-24

Family

ID=49322241

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013206019A Active JP6266290B2 (ja) 2012-12-05 2013-10-01 ガス・タービン・エンジンの燃焼器用燃料ノズル

Country Status (4)

Country Link
US (1) US9291103B2 (enExample)
EP (1) EP2741005B1 (enExample)
JP (1) JP6266290B2 (enExample)
CN (1) CN203744300U (enExample)

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US10094566B2 (en) * 2015-02-04 2018-10-09 General Electric Company Systems and methods for high volumetric oxidant flow in gas turbine engine with exhaust gas recirculation
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