Invention Grant
- Patent Title: Combustion chamber having a double chamber bottom
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Application No.: US16976354Application Date: 2019-02-28
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Publication No.: US11248793B2Publication Date: 2022-02-15
- Inventor: Jacques Marcel Arthur Bunel , Dan-Ranjiv Joory
- 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: FR1851784 20180228
- International Application: PCT/FR2019/050467 WO 20190228
- International Announcement: WO2019/166745 WO 20190906
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/28 ; F02C7/232
Abstract:
A gas turbo machine having a combustion chamber. The combustion chamber includes a chamber bottom having an upstream wall and a downstream wall extending between inner and outer annular walls. Each upstream and downstream walls each having openings for mounting fuel injection devices for injecting fuel through said openings. The downstream wall is sectorised.
Public/Granted literature
- US20210140639A1 COMBUSTION CHAMBER HAVING A DOUBLE CHAMBER BOTTOM Public/Granted day:2021-05-13
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