Invention Grant
- Patent Title: Centrifugal deaerator for a turbomachine
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Application No.: US16493161Application Date: 2018-03-07
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Publication No.: US11060456B2Publication Date: 2021-07-13
- Inventor: Benjamin Fulleringer , Jean-Pierre Pajard , Yannick Cazaux
- 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: FR1752306 20170321
- International Application: PCT/FR2018/050526 WO 20180307
- International Announcement: WO2018/172645 WO 20180927
- Main IPC: F02C7/06
- IPC: F02C7/06 ; F01D25/18 ; B01D45/14 ; F01M13/04 ; F02C7/32

Abstract:
A centrifugal deaerator for an air/oil mixture of a turbine engine includes: an annular housing arranged around a hollow shaft and having an outer annular wall and an inner annular wall; axial mixture inlets for the inflow of the air/oil mixture into annular housing; a pinion for rotating the annular housing, the pinion including a web that is securely connected to the hollow shaft and to the inner and outer annular walls; radial oil outlets in the outer wall; and oil-free air outlets in the inner wall. The axial mixture inlets and the radial oil outlets are axially arranged on either said of the web to prevent the axial mixture inlets from reintroducing oil evacuated by radial oil outlets into the annular housing.
Public/Granted literature
- US20200072126A1 CENTRIFUGAL DEAERATOR FOR A TURBOMACHINE Public/Granted day:2020-03-05
Information query
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