发明名称 |
GEARED TURBOFAN ENGINE WITH POWER DENSITY RANGE |
摘要 |
A gas turbine engine (120) has a high pressure turbine (130) configured to rotate with a high pressure compressor (126) as a high pressure spool (132) in a first direction about a central axis (C) and a low pressure turbine (134) configured to rotate with a low pressure compressor (124) as a low pressure spool (136) in the first direction about the central axis (C). A power density is greater than or equal to about 1.5 and less than or equal to about 5.5 lbf/cubic inches. A fan (122) is connected to the low pressure spool (136) via a speed changing mechanism (48) and rotates in a second direction opposed to the first direction. |
申请公布号 |
EP3043058(A1) |
申请公布日期 |
2016.07.13 |
申请号 |
EP20160150651 |
申请日期 |
2016.01.08 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SCHWARZ, FREDERICK M.;KUPRATIS, DANIEL BERNARD |
分类号 |
F02K3/06;F02C3/107 |
主分类号 |
F02K3/06 |
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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