发明名称 Retractable helicopter rotor
摘要 A retractable helicopter rotor in which the rotor and its blades, the swashplate and the pitch change rods are retracted and extended as a unit during the helicopter rotor retraction/extension mode of operation, wherein the connection between the rotor support system and the fuselage constitutes a single interface between overlapping circumferentially extending flanges of each, and with the bolts joining those flanges being loaded in compression.
申请公布号 US5149013(A) 申请公布日期 1992.09.22
申请号 US19910701257 申请日期 1991.05.16
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 COSTANZO, RALPH D.;DURWIN, ROBERT J.;HAGER, LEE N.;NOEHREN, WILLIAM L.
分类号 B64C27/32 主分类号 B64C27/32
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