Fuel spray nozzle for a gas turbine engine
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Mar 13, 2018
Issued Date -
N/A
app pub date -
Nov 25, 2014
filing date -
Dec 10, 2013
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
Nozzle for engine has coaxial arrangement of inner pilot and outer mains airblast fuel injectors and intermediate air-swirler passage sandwiched between the outer and inner air-swirler passages of the pilot and mains airblast fuel injectors, respectively. The nozzle has an annular first-splitter wall separating the pilot outer air-swirler passage from the intermediate one. An outer surface profile of the first-splitter wall defines radially inner side of the intermediate air-swirler passage. The nozzle has an annular second-splitter wall separating the intermediate air-swirler passage from mains inner air-swirler passage. An inner surface profile of second-splitter wall defines radially outer side of intermediate air-swirler passage. The outer and inner surface profile of the first and second splitters walls, respectively, have convergent sections facing each other forming convergent portion of the intermediate air-swirler passage. The inner surface profile of the second-splitter wall has a divergent section downstream of its convergent section.
First Claim
Other Claims data not available
Family
International Classification(s)
- 2014 Application Filing Year
- F23R Class
- 423 Applications Filed
- 330 Patents Issued To-Date
- 78.02 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 5 Citation Count
- F23R Class
- 12.28 % this patent is cited more than
- 7 Age
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