Invention Grant
- Patent Title: Heat exchanger comprising an inter-vane wall provided with hollow turbulence generators
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Application No.: US17757035Application Date: 2020-12-08
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Publication No.: US11753953B2Publication Date: 2023-09-12
- Inventor: Amélie Argie Antoinette Chassagne , Antoine Robert Alain Brunet , Cédric Zaccardi
- 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 14287 2019.12.12
- International Application: PCT/HR2020/052336 2020.12.08
- International Announcement: WO2021/116592A 2021.06.17
- Date entered country: 2022-06-08
- Main IPC: F01D9/06
- IPC: F01D9/06 ; F01D9/04 ; F01D25/14 ; F28F13/12 ; F28D21/00

Abstract:
An assembly for a turbomachine through which an air flow passes, includes a stator including guide vanes extending radially in relation to a longitudinal axis, at least one inter-vane platform extending between the radially outer ends of two circumferentially consecutive guide vanes, each inter-vane platform including an outer surface that faces the axis, a heat exchanger located downstream of the stator in relation to a direction of circulation of the air flow in the turbomachine during operation, this stator including a heat exchange surface extending in the extension of an inter-vane platform. At least one inter-vane platform located in the upstream extension of the heat exchange surface is provided with at least one turbulence generator on its outer surface.
Public/Granted literature
- US20230010301A1 HEAT EXCHANGER COMPRISING AN INTER-VANE WALL PROVIDED WITH HOLLOW TURBULENCE GENERATORS Public/Granted day:2023-01-12
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