发明名称 |
Bearing for aircraft engine rotor blade - incorporates torsional tie rod in compact design |
摘要 |
Bearing system for a swivel rotor blade fitted out with a holding journal which thrusts off the rotor disc via a swivel bearing. Centrifugal force is taken up by an inwards, easy-twisting tie rod whose free end is only secured on a radially inward part of the rotor disc (7, 2). The swivel bearing should be a radial bearing (6a, b) pref. composed of one or more needle bearings. The tie rod consists of a slit tube or fibre strand bundle or hollow rod. USE/ADVANTAGE - Aircraft engines, fan blades. Blade adjusting moment passed directly into journal, protected from centrifugal forces by torsional tie rod in compact design.
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申请公布号 |
DE4015207(C1) |
申请公布日期 |
1991.10.17 |
申请号 |
DE19904015207 |
申请日期 |
1990.05.11 |
申请人 |
MTU MOTOREN- UND TURBINEN-UNION MUENCHEN GMBH, 8000 MUENCHEN, DE |
发明人 |
HAIN, KLEMENS, DR., 8061 WIEDENZHAUSEN, DE;SCHUETTE, WILFRIED, 8024 OBERHACHING, DE |
分类号 |
F01D5/30;F01D7/00;F04D29/32 |
主分类号 |
F01D5/30 |
代理机构 |
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代理人 |
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