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HI-8597PSIF
+BOM-
제조업체Holt 집적 회로
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제조업체 부품 #HI-8597PSIF
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데이터시트 HI-8597PSIF DataSheet
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재고21276
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사양
| 속성 | 가치 |
| EU RoHS | Compliant |
| ECCN (US) | EAR99 |
| Part Status | Active |
| HTS | COMPONENTS |
| Automotive | No |
| PPAP | No |
| Minimum Operating Temperature (°C) | -40 |
| Maximum Operating Temperature (°C) | 85 |
| Mounting | Surface Mount |
| Package Height | 2.05(Min) |
| Package Width | 7.5 |
| Package Length | 10.3 |
| PCB changed | 16 |
| Standard Package Name | SO |
| Supplier Package | SOIC W EP |
| Pin Count | 16 |
| Lead Shape | Gull-wing |
| Maximum Supply Current (mA) | 40 |
| Power Supply Type | Single |
| Supplier Temperature Grade | Industrial |
| Function | Line Transmitter |
| Minimum Single Supply Voltage (V) | 3 |
| Typical Single Supply Voltage (V) | 3.3 |
| Maximum Single Supply Voltage (V) | 3.6 |
| SVHC | Yes |
| Number of Transmitters | 2 |
| Transmitter Signal Type | Differential |
| Number of Transmitter Enables | 2 |
| Data Transmission Topology | Point-to-Point |
| Driving Mode | 3-State |
개요
Description
1. Overview: A brief description of what HI-8597PSIF is—whether it's a piece of technology, a course code, or another type of identifier.
2. Purpose: Explanation of the product or course's primary function or objective. This could include its applications, target audience, or industry relevance.
3. Features/Content: Highlighting notable features, components, or topics covered, designed to provide users or students with a clear understanding of its capabilities or curriculum.
4. Benefits: Information on how it adds value, improves processes, or enhances knowledge in its respective field.
5. Usage: Any specific instructions, prerequisites, or recommendations for optimal use or understanding.
For accurate details, refer to the specific documentation or resources related to HI-8597PSIF.
Equivalent
1. Holt Integrated Circuits' HI-8596 or HI-8592 series.
2. Aeroflex's ACT429 family.
3. DDC's BU-6188 series.
It’s important to verify specific part requirements, including voltage levels and package types, to ensure compatibility.
Features
1. MIL-STD-1553 Compliance: Specifically designed to handle the protocol requirements of MIL-STD-1553B data buses, making it ideal for military and aerospace applications.
2. Dual Redundant Bus Interface: Supports a dual-redundant bus architecture, allowing for increased reliability and redundancy in critical communication systems.
3. Programmable Features: Offers programmable options for various operational modes, making it adaptable to different system requirements.
4. Low Power Consumption: Designed for efficient power usage, which is crucial for systems where power availability is limited.
5. High Integration: Combines multiple functions into a single chip to reduce the need for additional components, saving space and simplifying design.
6. Robust Design: Engineered to withstand harsh environmental conditions, including wide temperature ranges and electromagnetic interference.
7. Versatile Applications: Suitable for use in a variety of aerospace and defense systems, including aircraft, satellites, and ground vehicles.
These features make the HI-8597PSIF a versatile and reliable choice for advanced avionics systems.
Pinout
The pin configuration typically includes connections for the MIL-STD-1553 bus lines, power supply, ground, and digital control inputs/outputs for data transmission and reception. Specific pins will be designated for functions such as Bus A and Bus B differential signal lines, digital data input/output, transmit enable, and receive enable. There may also be pins for mode control and other operational settings, depending on the specific configuration and application requirements.
For precise pin functions and layout, referring to the manufacturer's datasheet is essential, as it provides detailed information on each pin's role and electrical characteristics.
Manufacturer
Application
1. Aircraft Data Communication: Facilitates communication between avionics systems using the ARINC 429 protocol.
2. Flight Control Systems: Helps in data exchange for flight management and control applications.
3. Navigation Systems: Assists in interfacing with navigation equipment for precise data transfer.
4. Aircraft Monitoring: Used for real-time monitoring and diagnostics.
5. Simulation and Testing: Applied in the development and testing of avionics systems.
These applications leverage the IC's ability to handle multiple ARINC 429 channels effectively, ensuring reliable data transfer across critical aviation systems.