- Patent Title: Turbine engine stator vane, fan casing comprising such a vane, thrust reverser system of a turbine engine equipped with such a vane and turbine engine equipped with said vane, said casing or said system
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Application No.: US15351790Application Date: 2016-11-15
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Publication No.: US10676204B2Publication Date: 2020-06-09
- Inventor: Kevin Morgane Lemarchand , Guillaume Olivier Vartan Martin
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@49c5b1fd
- Main IPC: F02K1/70
- IPC: F02K1/70 ; B64D33/04 ; F01D17/16 ; F04D29/54
Abstract:
A variable-orientation stator vane of a turbine engine, comprising a wall that extends between a leading edge and a trailing edge forming a chord line. The chord line increases from a root end towards a tip end of said vane. This vane is fitted pivotably in a turbine engine casing so as to divert a flow of cold air circulating in an annular duct thereof.
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