US Patent 7475546 Augmentor pilot nozzle
Patent 7475546 was granted and assigned to United Technologies on January, 2009 by the United States Patent and Trademark Office.
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Patent abstract
A gas turbine engine augmentor nozzle has an inlet for connection to an augmentor fuel conduit and an outlet for expelling a spray of fuel. A passageway between the inlet and outlet is at least partially bounded by outlet end surface portions diverging from each other. The nozzle may be used as a replacement for a non-divergent nozzle and may reorient a fuel jet centerline toward radial.
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US Patent 07475546 Augmentor pilot nozzle US Patent 7475546 Augmentor pilot nozzle
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Patent Number
0747554600
Patent Number
747554600
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Official Website
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
074755460
Date of Patent
January 13, 2009
0Patent Application Number
112311810
Date Filed
September 20, 2005
0Official Website
Patent Primary Examiner
Edits on 23 Sep, 2022
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
074755460
Date of Patent
January 13, 2009
0Patent Application Number
112311810
Date Filed
September 20, 2005
0Official Website
Patent Primary Examiner
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US Patent 07475546 Augmentor pilot nozzle
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
07475546
Date of patent
January 13, 2009
Patent application number
11231181
Date Filed
September 20, 2005
Patent primary examiner
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