Invention Grant
- Patent Title: Fuel injection device for a turbojet engine afterburner
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Application No.: US18555930Application Date: 2022-04-15
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Publication No.: US12104793B2Publication Date: 2024-10-01
- Inventor: Pierre André Gabriel Malbois
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pearne & Gordon LLP
- Priority: FR 03991 2021.04.19
- International Application: PCT/FR2022/050716 2022.04.15
- International Announcement: WO2022/223916A 2022.10.27
- Date entered country: 2023-10-18
- Main IPC: F23R3/20
- IPC: F23R3/20 ; F02C7/18 ; F02C7/22 ; F02K3/10

Abstract:
A flame-holder device for a turbojet afterburner comprises an annular row of flame-holder arms, each having an inner branch having a free end and another end, and two outer branches which extend from the other end (52) and diverge from one another in a direction extending from the free end to the other end, such that the inner branch transitions radially outward into the two outer branches which diverge radially outward from one another in two opposing circumferential directions, thereby forming mutually approaching areas between consecutive flame-holder arms for enabling the flame to spread from arm to arm.
Public/Granted literature
- US20240200780A1 FUEL INJECTION DEVICE FOR A TURBOJET ENGINE AFTERBURNER Public/Granted day:2024-06-20
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