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AERIAL ARRANGEMENTS AND FEEDING SYSTEMS THEREFOR

机译:航空安排和收费系统

摘要

1332151 Aerials MARCONI CO Ltd 19 April 1971 [9 Jan 1970] 1078/70 Heading H4A An aerial feeding system comprises two hybrid circuits 5, 7, Fig. 2, which are interconnected by two variable phase shifters 11, 12. Input is applied to one input terminal of the hybrid circuit 5, the other input terminal being connected to a matching load 6, and outputs are obtained from the output terminals of the hybrid circuit 7 for differently oriented aerial arrays 3, 4. Each phase shifter 11 or 12 has separately controlled 90 degree and 180 degree phasing sections and commonly controlled 22À5 degrees and 45 degree phasing sections. The hybrid circuits 5, 7 are of the kind in which an input results in two equal outputs having a 90 degree phase difference. With this arrangement, either the aerial array 3 or the aerial array 4 may be energized by suitably setting the phase shifters 11, 12. For example, if the phase shifter 11 is set to 90 degrees and the phase shifter 12 is set to 270 degrees, the fraction of power fed via the former to the array 3 experiences a phase change of (90 degrees + 90 degrees) = 180 degrees, and the fraction of power fed via the latter experiences a phase change of (270 degrees + 90 degrees) = 360 degrees. The two fractions are thus of opposite phase, and the array 3 is not energized. The corresponding fractions fed to the array 4 are, however, in phase. If both phase shifters have the same setting, the array 3 will be energized, but not the array 4. In another embodiment, the commonly controlled sections of the two phase shifters are removed, and a third phase shifter is instead placed in the input to the first hybrid circuit (Fig. 3, not shown). Fig. 4 shows an arrangement in which four radiating elements 13 14, 23, 24, each cover a quadrant in azimuth and are energizable one at a time. A feed system comprises two sets of pairs of hybrid circuits 15, 17 and 25, 27 respectively interconnected via pairs of variable phase shifters 111, 112 and 211, 212. One input terminal of each of the hybrid circuits 15, 25 is connected to one output terminal of a hybrid circuit 5, and their other output terminals are connected to respective matching loads 16, 26. Input power to the feed system is connected through a variable phase shifter 113 to one input terminal of the hybrid circuit 5, the other input terminal of which is connected to a matching load 6. Two other hybrid circuits 9, 10 are provided, the output terminals of which are connected to respective ones of the radiating elements 13, 14, 23, 24 and the input terminals of each of which are connected one to an output terminal of the hybrid circuit 17 and the other to an output terminal of the hybrid circuit 27. If, for example, the radiating element 13 is to be energized, the phase shifters 111, 112, 211, 212 are set, respectively, to 0 degrees, 0 degrees, 90 degrees, 270 degrees. It is possible to use such an arrangement where the various radiating elements are adapted to transmit signals of different frequencies. In another arrangement, (Fig. 5, not shown) feeding systems are provided for use until a circular array of radiating elements of the kind described in Specification 1,171,626. There are four successive sets of elements a 1 to a n , b 1 to b n , c 1 to c n , d 1 to d n , which are grouped in units a 1 , b 1 , c 1 , d 1 &c. A feeding system allows any two adjacent elements of a unit to be energized. Thus, the elements a 1 , c 1 are coupled through one pair of hybrid circuits and variable phase shifters similar to those shown in Fig. 2, and the elements b 1 , d 1 are coupled through another pair. One input terminal of each of the hybrid circuits remote from the elements is connected to an amplitude control system and the other terminal is connected to a matching load. The amplitude control system comprises two hybrid circuits which are interconnected by variable phase shifters.
机译:1332151天线MARCONI CO Ltd 1971年4月19日[1970年1月9日] 1078/70标题H4A空中馈电系统包括两个混合电路5、7(图2),它们由两个可变移相器11、12互连。混合电路5的一个输入端子,另一输入端子连接到匹配负载6,并且从混合电路7的输出端子获得输出以用于不同取向的天线阵列3、4。每个移相器11或12具有分别控制90度和180度移相段以及共同控制的22‑5度和45度移相段。混合电路5、7是这样的类型,其中输入导致两个具有90度相位差的相等输出。通过这种布置,可以通过适当地设置移相器11、12来给天线阵列3或天线阵列4通电。例如,如果将移相器11设置为90度并且将移相器12设置为270度。 ,通过前者馈入阵列3的功率部分经历了(90度+ 90度)= 180度的相变,而通过后者而馈入的功率部分经历了(270度+ 90度)的相变= 360度。因此,这两个部分是反相的,并且阵列3没有被激励。但是,送入阵列4的相应部分是同相的。如果两个移相器具有相同的设置,则将为阵列3供电,但不会为阵列4供电。在另一个实施例中,将两个移相器的共同控制部分去掉,而将第三个移相器放置在输入端中。第一混合电路(图3,未示出)。图4示出了一种布置,其中四个辐射元件13、14、23、24每个覆盖方位角的象限并且一次可激励。馈电系统包括两组分别通过可变移相器对111、112和211、212互连的成对的混合电路对15、17和25、27。每个混合电路15、25的一个输入端子连接到一个混合电路5的输出端子和它们的其他输出端子连接到相应的匹配负载16、26。馈电系统的输入功率通过可变移相器113连接到混合电路5的一个输入端子,另一输入其末端连接到匹配负载6。还提供了另外两个混合电路9、10,其输出端子分别连接到辐射元件13、14、23、24中的每个,以及每个辐射元件的输入端子。它们分别连接到混合电路17的输出端子,而另一个连接到混合电路27的输出端子。例如,如果要辐射辐射元件13,则移相器111、112、211、212是设置,尊重ely,分别为0度,0度,90度,270度。可以使用这样的布置,其中各种辐射元件适于发送不同频率的信号。在另一种布置中(图5,未示出),提供供使用的系统,直到在规格1171626中描述的那种类型的辐射元件的圆形阵列。有四组连续的元素a 1至a n,b 1至b n,c 1至c n,d 1至d n,它们按单元a 1,b 1,c 1,d 1&c分组。馈电系统允许单元的任何两个相邻元件通电。因此,元件a 1,c 1通过一对类似于图2所示的混合电路和可变移相器耦合,并且元件b 1,d 1通过另一对耦合。每个混合电路中远离元件的一个输入端子连接到振幅控制系统,另一端子连接到匹配负载。振幅控制系统包括两个混合电路,它们通过可变移相器互连。

著录项

  • 公开/公告号GB1332151A

    专利类型

  • 公开/公告日1973-10-03

    原文格式PDF

  • 申请/专利权人 MARCONI CO LTD;

    申请/专利号GBD1332151

  • 发明设计人

    申请日1971-04-19

  • 分类号H01Q3/24;

  • 国家 GB

  • 入库时间 2022-08-23 06:34:42

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