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<strong>Design</strong>ing with L and C Inverters 289<br />

Note the difference in L, and L\. The nomenclature is significant; henceforth,<br />

only prototype (synchronous resonator) reactances will have roman<br />

subscripts. Table 8.1 shows the final element values for the band-center<br />

frequency <strong>of</strong> 50 MHz. It is in the format for running analysis Program B4-1<br />

(Section 4.1.4). Several results are provided in Table 8.1. The 90-degree nodal<br />

phase relationship shown in Figure 8.12c was also confirmed.<br />

8.2.5. Summary <strong>of</strong> De.,igning With Simple Lande Inverters. The ABCD<br />

chain matrix for a pi arrangement <strong>of</strong> L's or C's was obtained for the case<br />

where both shunt branches were negative elements. Comparison with the<br />

ABCD matrix <strong>of</strong> a lossless, 90-degree transmission line revealed that these pi<br />

inverters are 90 degrees long at all frequencies and have characteristic impedances<br />

(Zo) that are proportional or inversely proportional to frequency for<br />

Land C inverters, respectively. It was also shown that the magnetic transformer<br />

equivalent circuit incorporates an inductive inverter with shunt inductances<br />

left over on each side. When these shunt inductances constitute the<br />

total synchronous nodal inductances, then the coupling coefficient K'j (flux<br />

linkage) between windings is (QLiQLj)-1/2 between the coupled nodes.<br />

The prototype asymptotic selectivity estimate that was connected with a<br />

breakpoint graph in Section 8.1.4 was modified to account for inverter<br />

frequency dependence. It turned out that each inductive inverter added 6<br />

dB/octave to the upper stopband slope and subtracted that amount in the<br />

lower stop band. Also, capacitive inverters affected the slope in the opposite<br />

manner. This comprehensive estimate <strong>of</strong> stopband selectivity is valid for<br />

frequencies greater than 1.2f o (geometrically symmetric about the tune frequency)<br />

or for losses greater than about 20 dB. Program A8-l was furnished<br />

to make the selectivity estimate from any set <strong>of</strong> dependent variables in order<br />

to find the remaining variable. An extended example <strong>of</strong> program utilization<br />

was included.<br />

Finally, a complete design example for a three-resonator filter was furnished.<br />

It contained all the major steps in direct-coupled filter design; subsequent<br />

refinements will not alter this fundamental procedure. <strong>Design</strong> success<br />

was confirmed by analysis using Program B4-1; the desired selectivity and<br />

impedance match were obtained. The choice <strong>of</strong> loaded-Q distribution in the<br />

ratios 1,2, 1 anticipated the maximally flat response described in Section 8.5.<br />

However, any arbitrary loaded-Q distribution could have been used without<br />

affecting the selectivity and impedance-matching outcome. Similarly, an arbitrary<br />

choice <strong>of</strong> resistance level within the filter provided acceptable element<br />

values. It was shown in Section 8.1.3 that such choices <strong>of</strong> resistance levels (and<br />

related inverter impedances) do not affect the selectivity or response shape.<br />

A rule was provided for checking any basic direct-coupled design: all the<br />

L's and C's touching a node should resonate. This check and the use <strong>of</strong> an<br />

analysis program justify carrying about five significant figures in calculations,<br />

even thOUgh such accuracy has little meaning in the real world <strong>of</strong> physical<br />

components. Otherwise, numerical or procedural mistakes are very easy to<br />

overlook.

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