发明名称 |
INLET PARTICLE SEPARATOR SYSTEM FOR A GAS TURBINE ENGINE |
摘要 |
Embodiments include an inlet particle separator system for a gas turbine engine. The inlet particle separator system includes an inertial particle separator that separates incoming air into a cleaned air flow and a scavenge flow. Embodiments may also include an ejector that provides a draw on a scavenge duct and entrains the scavenge flow into a charged flow, e.g., such as the output of a first stage fan. The ejector may have a variable output. |
申请公布号 |
EP2382026(A1) |
申请公布日期 |
2011.11.02 |
申请号 |
EP20090835497 |
申请日期 |
2009.12.05 |
申请人 |
ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC. |
发明人 |
LERG, BRYAN, H. |
分类号 |
B01D45/00;B01D45/06;F02C7/05;F02C7/052;F02C7/055;F02K3/02;F02K3/04 |
主分类号 |
B01D45/00 |
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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