Conical-flat heat shield for gas turbine engine combustor dome
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Jan 16, 2018
Issued Date -
N/A
app pub date -
Jun 25, 2015
filing date -
Jun 26, 2014
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A gas turbine engine combustor conical-flat heat shield includes an annular conical section extending upstream from and being integral with a flat section with a flat downstream facing surface which may be generally perpendicular to or canted with respect to a centerline. The flat section includes radially outer and inner edges at least one of which is circular and circumscribed about a centerline and circumferentially spaced apart clockwise and counter-clockwise radial edges having an origin on the centerline. A gas turbine engine combustor includes conical-flat heat shields in one or more circular rows arranged in a non-symmetrical or asymmetrical pattern. Two or more groups (A, B, C) of the conical-flat heat shields in the circular rows may be mounted on a domeplate and one or more of the conical-flat heat shields is different in one or more of the groups (A, B, C).
First Claim
Other Claims data not available
Family
International Classification(s)
- 2015 Application Filing Year
- F23R Class
- 450 Applications Filed
- 328 Patents Issued To-Date
- 72.89 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 1 Citation Count
- F23R Class
- 12.28 % this patent is cited more than
- 7 Age
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