Invention Grant
- Patent Title: Convergent-divergent nozzle for a turbine engine
-
Application No.: US14363508Application Date: 2012-12-04
-
Publication No.: US09683516B2Publication Date: 2017-06-20
- Inventor: Matthieu Leyko , Jean Bertucchi , Mathieu Gaillot
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1161282 20111207
- International Application: PCT/FR2012/052795 WO 20121204
- International Announcement: WO2013/083908 WO 20130613
- Main IPC: F02K1/00
- IPC: F02K1/00 ; F02K1/82 ; F02K3/06

Abstract:
A turbine engine convergent-divergent nozzle including an annular central element and an annular cap arranged coaxially around the central element to co-operate with the central element to define an annular flow channel for a gas stream from the engine. Between a throat section and an ejection section of the nozzle, the central element and the cap present respective internal profiles in longitudinal section that are modeled by curves having respective radii of curvature that are identical in absolute value.
Public/Granted literature
- US20150033747A1 CONVERGENT-DIVERGENT NOZZLE FOR A TURBINE ENGINE Public/Granted day:2015-02-05
Information query