Invention Grant
- Patent Title: Turbomachine with coaxial propellers
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Application No.: US17264234Application Date: 2019-07-26
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Publication No.: US11542891B2Publication Date: 2023-01-03
- Inventor: Adrien Dubois , Anthony Binder , Laurence Francine Vion
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Womble Bond Dickinson (US) LLP
- Priority: FR1857285 20180803
- International Application: PCT/FR2019/051856 WO 20190726
- International Announcement: WO2020/025886 WO 20200206
- Main IPC: F02K3/072
- IPC: F02K3/072 ; F02C6/08

Abstract:
The invention relates to a nubomachine with a longitudinal axis, comprising two, respectively upstream (122) and downstream, coaxial outer propellers (122), characterised in that at least some of the blades (148) of the upstream propeller (122) comprise at least one internal air circulation chimney (150) that communicates with air-bleeding openings (152) in tire boundary layers of the blades (148), and communicates with air outflow openings (158) on the radially outer end thereof, the air-bleeding openings (152) leading to opening inlets (152a) on tire passive surfaces (156) of the blades (148), the inlets (152a) of the air-bleeding openings being radially arranged in an area (H1) contained between 10% and 45% of the radial dimension (H2) of the blades (148), measured above turd from the radial height of the blades for which the tangent of the leading edge (138) of the blades is orthogonal to the longitudinal axis, and the inlets (152a) of the air bleeding openings being arranged in an area contained between 0% and 30% of the local chord of the blades (148), measured at the level of said inlets (152a) and from the leading edges (138) of tire blades (148).
Public/Granted literature
- US20210317799A1 TURBOMACHINE WITH COAXIAL PROPELLERS Public/Granted day:2021-10-14
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