- Patent Title: Profiled structure for an aircraft or turbomachine for an aircraft
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Application No.: US16657278Application Date: 2019-10-18
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Publication No.: US11560796B2Publication Date: 2023-01-24
- Inventor: Fernando Gea Aguilera , Raphaël Barrier , Mathieu Simon Paul Gruber , Cyril Polacsek , Hélène Dominique Jeanne Posson
- Applicant: SAFRAN AIRCRAFT ENGINES , OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
- Applicant Address: FR Paris; FR Palaiseau
- Assignee: SAFRAN AIRCRAFT ENGINES,OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
- Current Assignee: SAFRAN AIRCRAFT ENGINES,OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
- Current Assignee Address: FR Paris; FR Palaiseau
- Agency: Lathrop GPM LLP
- Priority: FR1859663 20181018
- Main IPC: F01D5/14
- IPC: F01D5/14 ; F01D9/04 ; B64C3/10 ; B64C21/10 ; B64C11/18

Abstract:
The invention relates to a profiled structure elongated in a direction in which the structure has a length exposed to an airflow and transversely to which the structure has a leading edge and/or a trailing edge, at least one of which is profiled and has, along said direction of elongation, geometric serration patterns defined by a succession of peaks and troughs. Along the profiled leading edge and/or trailing edge, the serration patterns have a geometric pattern that is repeated in the direction of elongation, the shape of which is stretched and/or contracted transversely to the direction of elongation and/or in the direction of elongation.
Public/Granted literature
- US20200148325A1 PROFILED STRUCTURE FOR AN AIRCRAFT OR TURBOMACHINE FOR AN AIRCRAFT Public/Granted day:2020-05-14
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