发明名称 |
GEARED TURBOFAN WITH IMPROVED GEAR SYSTEM MAINTAINABILITY |
摘要 |
A disclosed gas turbine engine includes a fan section including a hub supporting a plurality of fan blades rotatable about an axis, and a bearing assembly supporting rotation of the hub about the axis. A compressor section is in fluid communication with a combustor and a turbine is in fluid communication with the compressor section. A speed reduction device driven by the turbine section for rotating the fan about the axis is mounted forward of the bearing assembly supporting rotation of the hub. |
申请公布号 |
EP3084181(A1) |
申请公布日期 |
2016.10.26 |
申请号 |
EP20140872784 |
申请日期 |
2014.11.25 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SHERIDAN, WILLIAM G. |
分类号 |
F02C7/06;F01D25/16;F02K3/06;F16H1/28 |
主分类号 |
F02C7/06 |
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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