Invention Grant
- Patent Title: Turbine engine guide vane
-
Application No.: US14911626Application Date: 2014-08-04
-
Publication No.: US10221692B2Publication Date: 2019-03-05
- Inventor: Pradeep Cojande , Eric Pierre Maurice Lippinois , Hanna Reiss
- 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: FR1357956 20130812
- International Application: PCT/FR2014/052027 WO 20140804
- International Announcement: WO2015/022463 WO 20150219
- Main IPC: F01D5/14
- IPC: F01D5/14 ; F01D9/04 ; F04D29/54

Abstract:
An outlet guide vane for a turbine engine, the vane having a plurality of vane sections stacked along a radial axis Z. Over a bottom portion of the vane in the range 0 to 50% of its total height, the leading edge of each section is in front of the leading edge of the corresponding section at the total height, and the maximum thicknesses are located at positions that are offset from the leading edge by at least 50% of the chord.
Public/Granted literature
- US20160194962A1 TURBINE ENGINE GUIDE VANE Public/Granted day:2016-07-07
Information query