Invention Grant
- Patent Title: Combustion chamber of a turbine engine
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Application No.: US15916061Application Date: 2018-03-08
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Publication No.: US10684018B2Publication Date: 2020-06-16
- Inventor: Patrice André Commaret , Romain Nicolas Lunel
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Christensen O'Connor Johnson Kindness, PLLC
- Agent Ryan E. Dodge, Jr.
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@5c45e7da
- Main IPC: F23R3/06
- IPC: F23R3/06 ; F23R3/50 ; F23R3/00 ; F23R3/10

Abstract:
An annular combustion chamber with an axis of revolution of a turbine engine delimited by coaxial inner and outer annular walls joined upstream by a substantially transverse bottom of the chamber, the chamber further comprising at least one annular deflector placed in the chamber and substantially parallel to the bottom of the chamber the bottom of the chamber having orifices designed to be passed through by the impact cooling air of the deflector and coming from upstream. The deflector is attached to the inner and outer walls in a sealed manner, and the cooling air of the deflector is discharged from the chamber through exhaust holes formed in the inner and outer walls.
Public/Granted literature
- US20180266690A1 COMBUSTION CHAMBER OF A TURBINE ENGINE Public/Granted day:2018-09-20
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