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.
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
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