发明名称 |
Counterbalanced fuel slinger in a gas turbine engine |
摘要 |
A rotary fuel slinger and a turbine engine including the rotary fuel source is provided. The rotary fuel slinger includes a coupler shaft coupled to a turbine shaft of the turbine engine and is configured to rotate therewith. The slinger further includes a slinger disc coupled to the coupler shaft and configured to rotate therewith. The slinger disc includes a vertical shoulder extending substantially perpendicular to the coupler shaft and a slinger disc rim extending substantially perpendicularly from the vertical shoulder. The slinger disc rim is configured to define a cup-shaped section and a counterbalance mass, wherein the cup-shaped section is counterbalanced by the counterbalance mass. The rotary fuel slinger is adapted to receive a rotational drive force and to receive a flow of fuel from a fuel source and configured, upon receipt of the rotational drive force, to centrifuge the received fuel into a combustion chamber of the turbine engine.
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申请公布号 |
US2007234725(A1) |
申请公布日期 |
2007.10.11 |
申请号 |
US20060393580 |
申请日期 |
2006.03.29 |
申请人 |
HONEYWELL INTERNATIONAL, INC. |
发明人 |
CRITCHLEY IAN L.;HADDER JAMES L. |
分类号 |
F02C7/22 |
主分类号 |
F02C7/22 |
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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