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ACT4808 数据表(PDF) 2 Page - Aeroflex Circuit Technology

部件名 ACT4808
功能描述  ACT4808 DUAL TRANSCEIVERS FOR MACAIR A3818, A5690, A5232, A4905 & MIL-STD-1553
PDF  8 Pages
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制造商  AEROFLEX [Aeroflex Circuit Technology]
网页  http://www.aeroflex.com
标志 AEROFLEX - Aeroflex Circuit Technology

ACT4808 数据表(HTML) 2 Page - Aeroflex Circuit Technology

  ACT4808 Datasheet HTML 1Page - Aeroflex Circuit Technology ACT4808 Datasheet HTML 2Page - Aeroflex Circuit Technology ACT4808 Datasheet HTML 3Page - Aeroflex Circuit Technology ACT4808 Datasheet HTML 4Page - Aeroflex Circuit Technology ACT4808 Datasheet HTML 5Page - Aeroflex Circuit Technology ACT4808 Datasheet HTML 6Page - Aeroflex Circuit Technology ACT4808 Datasheet HTML 7Page - Aeroflex Circuit Technology ACT4808 Datasheet HTML 8Page - Aeroflex Circuit Technology  
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Aeroflex Circuit Technology
SCD4808 REV E 12/9/99
Plainview NY (516) 694-6700
2
inputs are held low or high, the
transmitter output becomes a high
impedance and is “removed” from
the line. In addition, an overriding
“INHIBIT" input provides for the
removal of the transmitter output
from the line. A logic “1” applied to
the “INHIBIT” takes priority over the
condition of the data inputs and
disables
the
transmitter.
(See
Transmitter
Logic
Waveforms,
Figure 1.)
The transmitter utilizes an active
filter to suppress harmonics above
1 MHz to meet Macair specifications
A-3818,
A-4905,
A-5232
and
A-5690. The transmitter may be
safely operated for an indefinite
period at 100% duty cycle into a
data bus short circuit (Pt. A-A’).
Receiver
The
Receiver
section
accepts
bi-phase differential data at the input
and produces two TTL signals at the
output. The outputs are DATA and
DATA, and represent positive and
negative excursions of the input
beyond a pre-determined threshold.
(See Receiver Logic Waveforms,
Figure 2.)
The internal threshold is nominally
set
to
detect
data
bus
signals
exceeding 1.10 Volts P-P and reject
signals less than 0.6 Volts P-P
when used with a 1:1 turns ratio
transformer. (See Figure 4 for
transformer
data
and
typical
connection.)
A low level at the Strobe input
inhibits
the
DATA
and
DATA
outputs.
DATA IN
DATA IN
INHIBIT
LINE TO LINE
OUTPUT
NOTES:
2. DATA and DATA inputs must be complementary waveforms or 50% duty cycle average, with no delays between them.
3. DATA and DATA must be in the same state during off time (both high or low).
Figure 1 – Transmitter Logic Waveforms
Figure 2 – Receiver Logic Waveforms
Note overlap
NOTE: Waveforms shown are for normally low devices. For normally high receiver output
devices, the receiver outputs are swapped as shown by the dashed lines
level
LINE TO LINE
INPUT
DATA OUT
DATA OUT
1. Line to line waveforms illustrate Macair signals, MIL-STD-1553 signals are trapezoidal



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