发明名称 |
Gas turbine engine assembly and methods of assembling same |
摘要 |
<p>A method facilitates assembling a gas turbine engine (10). The method comprises coupling a low-pressure turbine rotatable (14) about a drive shaft (32) to a counter-rotating fan assembly (16) including a first fan assembly (50) and a second fan assembly (52) wherein the first fan assembly rotates in a first direction (80) and the second fan assembly rotates in an opposite second direction (82). The method also comprises coupling a radial gearbox (100) substantially circumferentially about the drive shaft such that an input (104) of the gearbox is coupled to the low-pressure turbine and an output (106) of the gearbox is coupled to the counter-rotating fan assembly, and such that the gearbox is positioned within a lubrication fluid sump (170) that substantially circumscribes the gearbox.
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申请公布号 |
EP1777391(A3) |
申请公布日期 |
2014.01.22 |
申请号 |
EP20060255269 |
申请日期 |
2006.10.12 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
MONIZ, THOMAS ORY;ORLANDO, ROBERT JOSEPH |
分类号 |
F02C3/073;F01D25/18;F01D25/20;F02C7/06;F02C7/32;F02C7/36;F02K3/072 |
主分类号 |
F02C3/073 |
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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