Invention Grant
- Patent Title: Combustion chamber for a turbomachine
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Application No.: US16433078Application Date: 2019-06-06
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Publication No.: US11242994B2Publication Date: 2022-02-08
- Inventor: Yvan Yoann Guezel , François Xavier Chapelle , 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: Blank Rome LLP
- Priority: FR1854962 20180607
- Main IPC: F23R3/14
- IPC: F23R3/14 ; F23R3/28 ; F23R3/00

Abstract:
A combustion chamber for a turbomachine having a bottom wall, at least one mixing bowl for promoting the mixing of air and fuel, mounted in an opening in the bottom wall, at least one annular baffle mounted axially downstream of the bottom wall, with respect to the direction of the gas flow within the combustion chamber, around the opening. The baffle is produced in one piece with the mixing bowl so as to form a one-piece assembly that has at least one channel for the flow of cooling air. The channel has an air inlet located upstream of the bottom wall and an air outlet located downstream of the bottom wall. The air outlet is located radially opposite the baffle.
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