Invention Grant
- Patent Title: Turbine engine vane with asymmetrical profile
-
Application No.: US14511624Application Date: 2014-10-10
-
Publication No.: US09784112B2Publication Date: 2017-10-10
- Inventor: Maxime Briend , Sebastien Pautard
- Applicant: SNECMA , SAFRAN
- Applicant Address: FR Paris FR Paris
- Assignee: SNECMA,SAFRAN
- Current Assignee: SNECMA,SAFRAN
- Current Assignee Address: FR Paris FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1359878 20131011
- Main IPC: F01D25/00
- IPC: F01D25/00 ; F01D9/02 ; F01D5/14 ; F01D5/28
Abstract:
The invention relates to a turbine engine vane comprising a main body made of composite material, a leading edge, a trailing edge, and at least one metal structural reinforcement, the structural reinforcement comprising a junction surface portion connected to the main body, the structural reinforcement extending between the junction surface portion and one of the leading or trailing edges, the vane being characterized in that the profile of the junction surface portion of the structural reinforcement has a camber less than 30%.
Public/Granted literature
- US20150104299A1 TURBINE ENGINE VANE WITH ASYMMETRICAL PROFILE Public/Granted day:2015-04-16
Information query
