发明名称 Mechanism for turbine engine start from low spool
摘要 A gas turbine engine (10) includes a high spool (14), a low spool (12) mechanically connected to a fan (26, 28), a gear system (24), an actuator (22; 22'), and a starter (50). The gear system is actuable to engage and disengage the low spool to and from the high spool. The actuator is connected to the gear system for selectively engaging and disengaging the gear system. The starter is connected to the low spool and can drive rotation of the high spool through the low spool when the gear system is engaged.
申请公布号 EP2540991(A2) 申请公布日期 2013.01.02
申请号 EP20120169823 申请日期 2012.05.29
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BERRYANN, ANDREW P.;SUCIU, GABRIEL L.
分类号 F01D19/00;F02C3/113;F02C7/36;F02K3/04 主分类号 F01D19/00
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