- 专利标题: GEARED GAS TURBINE ENGINE WITH OIL DEAERATOR AND AIR REMOVAL
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申请号: US18358524申请日: 2023-07-25
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公开(公告)号: US20230366330A1公开(公告)日: 2023-11-16
- 发明人: William G. Sheridan
- 申请人: Raytheon Technologies Corporation
- 申请人地址: US CT Farmington
- 专利权人: Raytheon Technologies Corporation
- 当前专利权人: Raytheon Technologies Corporation
- 当前专利权人地址: US CT Farmington
- 主分类号: F01D25/18
- IPC分类号: F01D25/18 ; B01D19/00 ; F01D25/20 ; F02C7/06
摘要:
A gas turbine engine has a fan drive turbine for driving a gear reduction. The gear reduction drives a fan rotor. A lubrication system supplies oil to the gear reduction, and includes a lubricant pump to supply an air/oil mixture to an inlet of a deaerator. The deaerator includes a separator for separating oil and air, delivering separated air to an air outlet, and delivering separated oil back into an oil tank. The separated oil is first delivered into a pipe outwardly of the oil tank, and then into a location beneath a minimum oil level in the tank. Air within the oil tank moves outwardly through an air exit into the deaerator. A method of designing a gas turbine engine is also disclosed.
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