发明名称 |
EPICYCLIC GEAR TRAIN |
摘要 |
A turbine engine (10) has a fan shaft (20) and at least one tapered bearing mounted on the fan shaft (20). The fan shaft (20) includes at least one passage extending in a direction having at least a radial component, and adjacent the at least one tapered bearing. A fan (18) is mounted for rotation on the tapered bearing. An epicyclic gear train (22) is coupled to drive the fan (18). The epicyclic gear train (22) includes a carrier (26) supporting intermediate gears (32) that mesh with a sun gear (30) and a ring gear (38) that surrounds and meshes with the intermediate gears (32). Each of the intermediate gears (32) are supported on a respective journal bearing (34). The epicyclic gear train (22) defines a gear reduction ratio of greater than or equal to about 2.3. A turbine section is coupled to drive the fan (18) through the epicyclic gear train (22) and has a fan drive turbine that includes a pressure ratio that is greater than about 5. The fan (18) includes a pressure ratio that is less than about 1.45, and a bypass ratio of greater than about ten. |
申请公布号 |
EP3130766(A1) |
申请公布日期 |
2017.02.15 |
申请号 |
EP20160183877 |
申请日期 |
2016.08.11 |
申请人 |
United Technologies Corporation |
发明人 |
McCUNE, Michael E.;PORTLOCK, Lawrence E.;SCHWARZ, Frederick M. |
分类号 |
F01D25/16;F02C7/06;F02C7/36;F02K3/06 |
主分类号 |
F01D25/16 |
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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