发明名称 Multifunction structurally integrated VHF-UHF aircraft antenna system
摘要 An antenna system utilizing an electrically conductive portion (16) of an aircraft structure to radiate and receive very-high-frequency (VHF) and ultra-high-frequency (UHF) radio signals over a wide frequency range without the need for an active tuner to accommodate frequency changes. An antenna element (22) is housed in a tail fin endcap section (20) and is positioned and shaped to form an elongated notch (26) between one edge (24) of the element itself and one adjacent edge (18) of an electrically conductive tail fin (16). The notch (26) is uniform over part of its length and is flared to a wider spacing over the remainder of its length. A feed point (30) along the notch (26) is selected for optimum performance. Matching electronics (14) couple the antenna system to a transceiver (15), which can operate either in a VHF/FM band, or in a UHF band, or in a VHF/AM band. The antenna system provides relatively good gain over the frequency range and provides a practically omnidirectional radiation pattern.
申请公布号 US5825332(A) 申请公布日期 1998.10.20
申请号 US19960712686 申请日期 1996.09.12
申请人 TRW INC. 发明人 CAMACHO, GERARDO I.;CAMPBELL, DONN V.
分类号 H01Q19/22;H01Q1/22;H01Q1/28;H01Q3/26;H01Q9/40;H01Q13/10;H01Q21/29;H04B7/185;(IPC1-7):H01Q1/28 主分类号 H01Q19/22
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