发明授权
US08201664B2 Lubrication system and method, and vortex flow separator for use therewith
有权
润滑系统和方法,以及与其一起使用的涡流分离器
- 专利标题: Lubrication system and method, and vortex flow separator for use therewith
- 专利标题(中): 润滑系统和方法,以及与其一起使用的涡流分离器
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申请号: US12018376申请日: 2008-01-23
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公开(公告)号: US08201664B2公开(公告)日: 2012-06-19
- 发明人: Sylvain Brouillet , Pierre-Yves Légaré
- 申请人: Sylvain Brouillet , Pierre-Yves Légaré
- 申请人地址: CA Longueuil
- 专利权人: Pratt & Whitney Canada Corp.
- 当前专利权人: Pratt & Whitney Canada Corp.
- 当前专利权人地址: CA Longueuil
- 代理机构: Norton Rose Canada LLP
- 主分类号: F01M1/10
- IPC分类号: F01M1/10 ; B04C5/02
摘要:
An aircraft engine lubrication system has a vortex separator, a first pump line having a first pump, an inlet connected to a separated lubricant area at the outlet end of the separator, and an outlet connectable to the engine. A scavenge line is provided for returning lubricant from the engine to an inlet end of the separator. A lubricant tank is connected in fluid flow communication with the separator by a connection line. A second pump line having a second pump has an inlet connected to the lubricant tank and an outlet connected to the separator for pumping lubricant from the tank to the inlet end of the separator.
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