发明名称 |
LUBRICATION SYSTEM AND METHOD, AND VORTEX FLOW SEPARATOR FOR USE THEREWITH |
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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申请公布号 |
US2009183950(A1) |
申请公布日期 |
2009.07.23 |
申请号 |
US20080018376 |
申请日期 |
2008.01.23 |
申请人 |
BROUILLET SYLVAIN;LEGARE PIERRE-YVES |
发明人 |
BROUILLET SYLVAIN;LEGARE PIERRE-YVES |
分类号 |
F01M1/10;B04C5/02 |
主分类号 |
F01M1/10 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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