Garmin GDR 66, Инструкция по установке

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Page 4-4 GDR 66 Installation Manual
Revision A 190-00303-24
4.2 Power Functions
4.2.1 Aircraft Power
The GDR 66 provides two aircraft power bus inputs. Pins 28, 30, and 32 of P662 are internally connected
to form AIRCRAFT POWER 1. Pins 34, 36, and 38 of P662 are internally connected to form AIRCRAFT
POWER 2. AIRCRAFT POWER 1 and AIRCRAFT POWER 2 are “diode ORed” to provide power
redundancy. Use of three AIRCRAFT POWER pins (either AIRCRAFT POWER 1 or AIRCRAFT
POWER 2) and three POWER GROUND pins is recommended for all installations.
4.2.2 Remote Power Off
The GDR 66 powers down when the COM REMOTE POWER OFF input is active. COM REMOTE
POWER OFF is a non-configurable discrete input conforming to:
Low: 0 VDC < Vin < 3.5 VDC, OR Rin > 100k ohms (inactive)
High: 8 VDC < Vin < 36 VDC (active)
4.2.3 GDR System ID Program
The GDR 66 determines it’s unit number based on the status of three GDR SYSTEM ID PROGRAM*
non-configurable discrete inputs conforming to:
Low: 0 VDC < Vin < 3.5 VDC, OR Rin < 375 ohms (active)
High: 8 VDC < Vin < 36 VDC, OR Rin > 100k ohm (inactive)
Table 4-3 Aircraft Power
Pin Name Connector Pin I/O
AIRCRAFT POWER 1 P662 28 In
AIRCRAFT POWER 1 P662 30 In
AIRCRAFT POWER 1 P662 32 In
AIRCRAFT POWER 2 P662 34 In
AIRCRAFT POWER 2 P662 36 In
AIRCRAFT POWER 2 P662 38 In
POWER GROUND P662 1 --
POWER GROUND P662 24 --
POWER GROUND P662 26 --
POWER GROUND P662 40 --
POWER GROUND P662 42 --
POWER GROUND P662 43 --
Table 4-4 Remote Power Off
Pin Name Connector Pin I/O
COM REMOTE POWER OFF P661 16 In
Table 4-5 System ID Program
Pin Name Connector Pin I/O
GDR SYSTEM ID PROGRAM* 1 P661 20 In
GDR SYSTEM ID PROGRAM* 2 P661 22 In
GDR SYSTEM ID PROGRAM* 3 P661 24 In
DRAFT