发明名称 |
CANTILEVERED TIP TURBINE ENGINE |
摘要 |
<p>A tip turbine engine (10) according to the present invention includes an engine support structure (12) for cantilevering a load bearing shaft from an engine support plane (P). An engine support structure (12) defines the engine support plane (P), which is perpendicular to an engine centerline (A). The shaft (60) is rotationally fixed, coaxial with the engine centerline (A), and structurally supported by the engine support structure (12) such that a load borne by the shaft (60) is transferred along the engine support plane.</p> |
申请公布号 |
EP1825112(B1) |
申请公布日期 |
2013.10.23 |
申请号 |
EP20040822088 |
申请日期 |
2004.12.01 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;ROBERGE, GARY D.;MERRY, BRIAN |
分类号 |
F02C3/073;F01D25/28;F02K3/068 |
主分类号 |
F02C3/073 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|