Invention Grant
- Patent Title: Grating for the formation of a reverse flow of an aircraft turbofan engine
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Application No.: US16201265Application Date: 2018-11-27
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Publication No.: US11028801B2Publication Date: 2021-06-08
- Inventor: Christophe Bourdeau , Quentin Vaucouloux , Romain Cusset
- Applicant: Airbus Operations SAS
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR1761914 20171211
- Main IPC: F02K1/72
- IPC: F02K1/72

Abstract:
A grating for the formation of a reverse flow of a turbofan engine and comprising fins of a first type having a curved profile whose rounding is oriented aft and whose center of curvature is forward relative to the fin of the first type, fins of a second type having a curved profile whose rounding is oriented aft and whose center of curvature is forward relative to the fin of the second type. In this grating, each fin of one of the two types is inserted between two fins of the other type moving from forward to aft and the cord of the fins of the second type is smaller than the cord of the fins of the first type.
Public/Granted literature
- US20200025138A1 GRATING FOR THE FORMATION OF A REVERSE FLOW OF AN AIRCRAFT TURBOFAN ENGINE Public/Granted day:2020-01-23
Information query
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