Combustion chamber with a hot compressed air deflector, in particular for a turbine intended for producing energy, in particular electrical energy
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United States of America Patent
Stats
-
Nov 2, 2021
Grant Date -
Jun 27, 2019
app pub date -
Jul 11, 2017
filing date -
Aug 29, 2016
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
The present invention relates to a combustion chamber (10) of a turbine, in particular a turbine with a thermodynamic cycle comprising a recuperator, for producing energy, in particular electrical energy, comprising a casing (12) with an injection means (52) for injecting at least one fuel, and a hot compressed air intake (32), said casing housing a flame tube (22) with a perforated diffuser (26) for the passage of the hot compressed air and the fuel, and a flame stabiliser (54). According to the invention, the chamber comprises an air deflector (36) arranged facing the hot compressed air intake (32) in order to circulate this hot air in a single axial direction from this intake.
First Claim
Other Claims data not available
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International Classification(s)
- 2017 Application Filing Year
- F02K Class
- 489 Applications Filed
- 321 Patents Issued To-Date
- 65.65 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 0 Citation Count
- F02K Class
- 0 % this patent is cited more than
- 4 Age
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