发明名称 |
HOLLOW COMPOSITE STRUCTURE USED AS WAVEGUIDE |
摘要 |
Embodiments of the invention include a system including a spar of a wing having an outer body defining a hollow cavity in the outer body, a first communication assembly including a receiver and a first antenna connected to the receiver for receiving one or both of electrical signals and power, the first antenna located in the hollow cavity, and a second communication assembly. The second communication assembly includes a second antenna located in the hollow cavity and an electrical device. The second communication assembly is configured to transmit, by the second antenna, one or both of electrical signals and power through the hollow cavity to the first antenna. |
申请公布号 |
WO2014168682(A1) |
申请公布日期 |
2014.10.16 |
申请号 |
WO2014US16040 |
申请日期 |
2014.02.12 |
申请人 |
SIKORSKY AIRCRAFT CORPORATION |
发明人 |
TOKGOZ, CAGATAY;SOLDNER, NICHOLAS CHARLES;ZACCHIO, JOSEPH |
分类号 |
H01Q1/28 |
主分类号 |
H01Q1/28 |
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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