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.
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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 |
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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