发明名称 |
Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and single direction of rotation booster aft of counter rotating fans |
摘要 |
<p>The assembly has a low pressure turbine with a flowpath and located aft of a high pressure spool (33). The low pressure turbine has counter rotatable low pressure inner and outer rotatable turbines. A single direction rotation booster has a row of booster blades connected to a low pressure outer shaft and axially located aft and downstream of a fan blade row (15).</p> |
申请公布号 |
EP1403500(A1) |
申请公布日期 |
2004.03.31 |
申请号 |
EP20030256033 |
申请日期 |
2003.09.25 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
ORLANDO, ROBERT JOSEPH;BAUGHMAN, JOHN LEWIS;MONIZ, THOMAS ORY |
分类号 |
F02C6/00;F01D1/24;F02C3/067;F02K3/072;(IPC1-7):F02K3/072 |
主分类号 |
F02C6/00 |
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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