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UT54ACS245S Datasheet(PDF) 1 Page - Aeroflex Circuit Technology

Part # UT54ACS245S
Description  Schmitt Octal Bus Transceiver with Three-State Outputs
PDF  10 Pages
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Manufacturer  AEROFLEX [Aeroflex Circuit Technology]
Direct Link  http://www.aeroflex.com
Logo AEROFLEX - Aeroflex Circuit Technology

UT54ACS245S Datasheet(HTML) 1 Page - Aeroflex Circuit Technology

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Standard Products
UT54ACS245S
Schmitt Octal Bus Transceiver with Three-State Outputs
Datasheet
November 2010
www.aeroflex.com/logic
FEATURES
Three-state outputs drive bus line directly
1.2μ CMOS
- Latchup immune
High speed
Low power consumption
Single 5 volt supply
Available QML Q or V processes
Flexible package
- 20-pin DIP
- 20-lead flatpack
UT54ACS245S - SMD 5962-96572
DESCRIPTION
The UT54ACS245S is a non-inverting octal bus transceiver with
Schmitt Trigger input levels. The circuit is designed for asyn-
chronous two-way communication between data buses. The
control function implementation minimizes external timing re-
quirements.
The device allows data transmission from the A bus to the B bus
or from the B bus to the A bus depending upon the logic level
at the direction control (DIR) input. The enable input (G) dis-
ables the device so that the buses are effectively isolated.
The device is characterized over full military temperature range
of -55
°C to +125°C.
FUNCTION TABLE
PINOUTS
20-Pin DIP
Top View
20-Lead Flatpack
Top View
LOGIC SYMBOL
ENABLE
G
DIRECTION
CONTROL DIR
OPERATION
L
L
B Data To A Bus
L
H
A Data To B Bus
H
X
Isolation
1
2
3
4
5
7
6
20
19
18
17
16
14
15
DIR
A1
A2
A3
A4
A5
A6
VDD
G
B1
B2
B3
B5
8
13
A7
B6
B4
9
12
A8
B7
10
11
VSS
B8
1
2
3
4
5
7
6
20
19
18
17
16
14
15
DIR
A1
A2
A3
A4
A5
A6
VDD
G
B1
B2
B3
B5
8
13
A7
B6
B4
9
12
A8
B7
10
11
VSS
B8
(19)
G
G3
(2)
A1
(3)
A2
(4)
(18)
B1
(16)
(17)
B2
Note:
1. Logic symbol in accordance with ANSI/IEEE Std 91-1984 and IEC
Publication 617-12.
A3
(5)
A4
(6)
A5
(7)
A6
B3
(13)
B6
(14)
B5
(15)
B4
(8)
A7
(9)
A8
(11)
B8
(12)
B7
(1)
DIR
3 EN1 (BA)
3 EN2 (AB)
1
2


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