SOUTHERN AVIONICS COMPANY
Model SA100 Dual
2-62
Theory of Operation, Radiobeacon
2.4 Detailed Circuit Analysis: Automatic Transfer
System SA Series
2.4.1 Local Radiobeacon Control System
See Figures "Local Radiobeacon Control System Overall Schematic" and "Local Radiobeacon
Control System Diagram" for schematic and diagram drawings of the Local Radiobeacon Control
System, Figures "Autotransfer Logic PWB Schematic" and "Autotransfer Logic PWB Diagram"
for schematic and diagram drawings of the Autotranfer Logic PWB, and Figure "Local Transfer
Indicator PWB Diagram" for the diagram drawing of the Local Transfer Indicator PWB.
Upon initial application of power to the Local Radiobeacon Control System or after pressing the
RESET pushbutton on the Control panel, the system will begin a sequence to first remove power
from the secondary transmitter, then switch the antenna relay to the primary transmitter, and
finally apply power to the primary transmitter. This is accomplished through logic contained on
the Autotransfer Logic PWB. U2 pin 3 of the Autotransfer Logic PWB will initially begin with 0 V.
This will force a logic 1 (5V) on U3 pin 1. U3 generates a fixed delay in the passage of a logic
signal. After approximately 0.6 seconds, the logic signal which is present at U3 pin 1 will appear
at U3 pins 12, 13. After an additional 0.6 seconds, the logic signal will appear at pin 6 of U3. The
logic signals from pins 1, 12 and 6 of U3 pass to U4 gates C, B and D, respectively, where they
will be inverted if the upper transmitter is selected as primary, or passed through without
inversion if the lower transmitter is selected as primary. The logic signals from gates B and C are
applied to U7 to set and re-set the flip-flops formed by U7 gates A, B, C and D. These control the
relay drivers for K2 and K3, the upper (Transmitter 1) and lower (Transmitter 2) transmitter power
relays respectively. The output of U4 gate D is applied through an inverting buffer of U6 to Q3,
the relay driver for antenna relay K1. After the primary transmitter receives operating power it will
respond with a 12 V sense signal to indicate proper transmitter operation. This signal, present at
pin 12 or 13 of the Autotransfer Logic PWB, will be coupled through gates A, B and C of U1 to U2
pin 5. The sense signal for the SA series transmitters is approxi12 volts.
With a logic 1 now present at U2 pin 5, a logic 0 will be present at pins 3 and 4, and a logic 1 at
pin 2. The transfer unit will thus be latched into the primary transmitter mode. A failure within the
primary transmitter, signaled by a drop in the sense line voltage from 12 V to 0 V, will produce a
logic 0 at U2 pin 5, a logic 1 at pins 3 and 4, and a logic 0 at pin 2. As the logic 0 now present at
U3 pin 1 is passed through the two delays of U3, the transfer logic will first remove power from
the primary transmitter, then transfer antenna connections to the secondary transmitter. The
removal of power from the primary transmitter prevents a reapplication of the 12 V sense signal
and latches the transfer unit into the secondary mode. Logic gates in integrated circuits U2 and
U5 furnish indications of system status through the control panel Primary, Secondary and Fail
LED's.
The ON/OFF transmitter power switch is used to turn off or turn on the operating transmitter via
the Logic OFF/ON control signal applied to pin 18. The primary transmitter always comes on first
irrespective of whether the primary or secondary was working when the transmitter power was
turned OFF.
Fail Alarm relay K1 on the Autotransfer Logic PWB furnishes remote alarm capability through a 1
form C SPDT relay contact set. The relay is activated in primary or secondary mode, and
deactivated for fail mode or loss of operating power. The contacts are rated 1 amp at 115 VAC
with a resistive load.
Содержание SA100
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Страница 43: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 13 Theory of Operation Radiobeacon Figure 2 6 Tone Key PWB Diagram...
Страница 45: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 15 Theory of Operation Radiobeacon Figure 2 7 Audio PWB Schematic...
Страница 46: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 16 Theory of Operation Radiobeacon Figure 2 8 Audio PWB Diagram...
Страница 48: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 18 Theory of Operation Radiobeacon Figure 2 9 ACTRL Schematic...
Страница 49: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 19 Theory of Operation Radiobeacon Figure 2 10 ACTRL Diagram...
Страница 53: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 23 Theory of Operation Radiobeacon Figure 2 13 CRS Sample Program...
Страница 58: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 28 Theory of Operation Radiobeacon D Figure 2 17 DMOD PWB Diagram...
Страница 64: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 34 Theory of Operation Radiobeacon Figure 2 21 Filter PWB Diagram...
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Страница 70: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 40 Theory of Operation Radiobeacon Figure 2 26 AMTR Diagram...
Страница 73: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 43 Theory of Operation Radiobeacon Figure 2 29 Monitor PWB Diagram...
Страница 75: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 45 Theory of Operation Radiobeacon Figure 2 31 SA LED PWB Diagram...
Страница 82: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 52 Theory of Operation Radiobeacon Figure 2 37 DCHOKE PWB Diagram...
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Страница 110: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 80 Theory of Operation Radiobeacon Figure 2 59 Modem PWB Schematic...
Страница 111: ...SOUTHERN AVIONICS COMPANY Model SA100 Dual 2 81 Theory of Operation Radiobeacon Figure 2 60 Modem PWB Assembly...
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