发明名称 |
Method of assembling a gas turbine engine and rotor assembly |
摘要 |
A method facilitates assembling a gas turbine engine (10). The method comprises providing a rotor assembly (62) including a rotor shaft (26) and a rotor disk (66) that includes a radially outer rim (68), a radially inner hub (70), and an integral web (72) extending therebetween, wherein the rotor assembly is rotatable about an axis of rotation (28) extending through the rotor shaft, and coupling a disk retainer (82) including at least one discharge tube (164) to the rotor disk wherein the discharge tube extends outwardly from the disk retainer for pumping the air to a higher pressure before discharging cooling fluid therefrom in a direction that is substantially perpendicular with respect to the axis of rotation. |
申请公布号 |
EP1512843(B1) |
申请公布日期 |
2016.03.09 |
申请号 |
EP20040253920 |
申请日期 |
2004.06.30 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SIMEONE, PETER ANDREW;WIGON, JEREMY STEPHAN;IGLESIAS, DENNIS CENTENO;LENAHAN, DEAN THOMAS;ST. HILAIRE, ALAN PATRICK;MCGOVERN, JAMES PATRICK |
分类号 |
F01D5/08;F01D25/08;F01D5/02;F01D5/06;F01D5/14;F01D5/28;F01D5/30;F02C7/00;F02C7/18 |
主分类号 |
F01D5/08 |
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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