Invention Grant
- Patent Title: Turbomachine centrifugal breather component and method for manufacturing said component
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Application No.: US16648189Application Date: 2018-09-24
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Publication No.: US11938431B2Publication Date: 2024-03-26
- Inventor: Arnaud Nifenecker , Benjamin Fulleringer , Cédric Lempegnat , Samuel Jousselin , Pierre Gaymu , Cédric Georget , Rémi Lanquetin , Philippe Olharan
- Applicant: SAFRAN HELICOPTER ENGINES
- Applicant Address: FR Bordes
- Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee Address: FR Bordes
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: FR 58909 2017.09.26
- International Application: PCT/EP2018/075741 2018.09.24
- International Announcement: WO2019/063458A 2019.04.04
- Date entered country: 2020-03-17
- Main IPC: B01D45/14
- IPC: B01D45/14 ; B01D46/00 ; F01D25/18 ; F02C7/06 ; F16N39/00

Abstract:
A component for a centrifugal deaerator for removing gas from a turbomachine air/oil mixture includes a structural part configured to delimit a duct for the flow of the air/oil mixture, and includes a circumferential enclosure for the centrifugal separation of the air/oil mixture, an axial inlet for the air/oil mixture, radial oil outlets, and an outlet for oil-free air. The component includes at least one cellular structure configured to filter the oil while allowing the air to pass and occupying at least a space in the duct.
Public/Granted literature
- US20200222841A1 TURBOMACHINE CENTRIFUGAL BREATHER COMPONENT AND METHOD FOR MANUFACTURING SAID COMPONENT Public/Granted day:2020-07-16
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