US Patent 7694899 Fuel injection device for an aircraft gas turbine
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Patent abstract
A fuel injection device for fuel injection systems, e.g. for aircraft gas turbines, includes at least one fuel injection opening, through which a continuous flow of fuel 1 is issued, with the fuel injection opening having a non-circular cross-section.
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US Patent 07694899 Fuel injection device for an aircraft gas turbine US Patent 7694899 Fuel injection device for an aircraft gas turbine
Infobox
Patent Number
0769489900
Patent Number
769489900
Edits on 22 Apr, 2023
Golden AI
Infobox
Is a
Patent Jurisdiction
Patent Number
076948990
Date of Patent
April 13, 2010
0Patent Application Number
118262310
Date Filed
July 13, 2007
0Official Website
Patent Primary Examiner
Edits on 23 Sep, 2022
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Infobox
Is a
Patent Jurisdiction
Patent Number
076948990
Date of Patent
April 13, 2010
0Patent Application Number
118262310
Date Filed
July 13, 2007
0Official Website
Patent Primary Examiner
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US Patent 07694899 Fuel injection device for an aircraft gas turbine
Infobox
Is a
Patent jurisdiction
Patent number
07694899
Date of patent
April 13, 2010
Patent application number
11826231
Date Filed
July 13, 2007
Patent primary examiner
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