发明名称 |
FAN BLADE ASSEMBLY FOR A TIP TURBINE ENGINE AND METHOD OF ASSEMBLY |
摘要 |
<p>A tip turbine engine comprises a fan-turbine rotor assembly that includes one or more turbine ring rotors. Each turbine ring is assembled from a multitude of turbine blade clusters. Assembly of a multitude of turbine blade clusters to a diffuser includes axial installation and radial rotation. The clusters are axially installed, then rotated toward a radial stop in a direction which will maintain each cluster against the radial stop during operation of the fan-turbine rotor assembly. A multitude of turbine rotor ring stages may also be locked together to future increase the rigidity of the turbine.</p> |
申请公布号 |
EP1834067(B1) |
申请公布日期 |
2008.11.26 |
申请号 |
EP20040822135 |
申请日期 |
2004.12.01 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;NORRIS, JAMES W.;NORDEEN, CRAIG A. |
分类号 |
F01D5/22;F01D5/30;F02C3/073;F02C3/08;F02K3/068 |
主分类号 |
F01D5/22 |
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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