Invention Grant
- Patent Title: Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face
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Application No.: US16381326Application Date: 2019-04-11
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Publication No.: US11274632B2Publication Date: 2022-03-15
- Inventor: Jonathan Langridge , Julien Szydlowski
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1357107 20130718
- Main IPC: F02K1/44
- IPC: F02K1/44 ; F02K1/34 ; F02K1/38 ; F02K1/46

Abstract:
In a cowl for a nozzle, an internal wall has a cross-section with a determined abscissa on the axis defining a neck line on the internal wall. The cowl has, downstream of the determined abscissa, indentations in the trailing edge which delimit chevrons distributed in the circumferential direction. The internal wall of the cowl diverges radially towards the interior, in a second axial half-plane passing through the tip of a chevron, from the upstream tangent on the point of the neck line in the second axial half-plane, and the lines defining the internal wall of the cowl in any axial half-plane do not have a turning point downstream of the determined abscissa of the neck line.
Public/Granted literature
- US20190234345A1 NOZZLE OF A TURBOMACHINE PROVIDED WITH CHEVRONS WITH A NON-AXISYMMETRIC INNER FACE Public/Granted day:2019-08-01
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