Texas Instruments SN74ABT16833DGGR

ROHS3Compliant Obsolete Transceiver Non-Inverting Push-Pull logic receiver -40C~85C TA 4.5V~5.5V 32mA 64mA
$ 1.901
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Texas Instruments

Datasheet13 pagesIl y a 18 ans

Sierra IC

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Pièces détachées

Registered Bus Transceiver, ABT Series, 2-Func, 8-Bit, True Output, BICMOS, PDSO56
Registered Bus Transceiver, ABT Series, 2-Func, 8-Bit, True Output, BICMOS, PDSO56
8 64mA 4.5V~5.5V 32mA 2 TSSOP-56 Buffer/Driver/Transceiver ROHS
Texas InstrumentsSN74LVC16646ADGVR
16-Bit Bus Transceiver And Register With 3-State Outputs 56-TVSOP -40 to 85
2 8 2.7V 3.6V 24mA Non-Inverting,Transceiver 8mA TVSOP-48 9.7mm*4.4mm*1mm

Descriptions

Descriptions de Texas Instruments SN74ABT16833DGGR fournies par ses distributeurs.

ROHS3Compliant Obsolete Transceiver Non-Inverting Push-Pull logic receiver -40C~85C TA 4.5V~5.5V 32mA 64mA
ABT SERIES DUAL 8-BIT TRANSCEIVER TRUE OUTPUT PDSO56
Bus XCVR Dual 16-CH 3-ST 56-Pin TSSOP T/R
IC DUAL 8-9BIT BUS TXRX 56-TSSOP
IC TXRX NON-INVERT 5.5V 56TSSOP
DUAL 8-BIT TO 9-BIT PARITY BUS TRANSCEIVERS
The 'ABT16833 consist of two noninverting 8-bit to 9-bit parity bus transceivers and are designed for communication between data buses. For each transceiver, when data is transmitted from the A bus to the B bus, an odd-parity bit is generated and output on the parity I/O pin (1PARITY or 2PARITY). When data is transmitted from the B bus to the A bus, 1PARITY (or 2PARITY) is configured as an input and combined with the B-input data to generate an active-low error flag if odd parity is not detected. The error (1 or 2) output is configured as an open-collector output. The B-to-A parity-error flag is clocked into 1 (or 2) on the low-to-high transition of the clock (1CLK or 2CLK) input. 1 (or 2) is cleared (set high) by taking the clear (1 or 2) input low. The output-enable ( and) inputs can be used to disable the device so that the buses are effectively isolated. When both and are low, data is transferred from the A bus to the B bus and inverted parity is generated. Inverted parity is a forced error condition that gives the designer more system diagnostic capability. To ensure the high-impedance state during power up or power down, should be tied to VCC through a pullup resistor; the minimum value of the resistor is determined by the current-sinking capability of the driver. The SN54ABT16833 is characterized for operation over the full military temperature range of -55°C to 125°C. The SN74ABT16833 is characterized for operation from -40°C to 85°C.

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  • TEXAS INSTUMENTS
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  • Texas Instruments Inc.