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CCC TIOC-555HD Triple Modular Redundant (TMR) Input/Output Controller

Parameter Name
Parameter Value
Product Model
CCC TIOC-555HD
Manufacturer
Curtiss-Wright Controls
Product Type
Triple Modular Redundant (TMR) Input/Output Controller
Architecture
Triple Modular Redundancy (TMR)​ with 2-out-of-3 (2oo3) voting on all critical I/O channels. Three independent, synchronized channels (A, B, C) operate in lockstep.
Category: Product ID: 23431

Description

Product Overview

The CCC TIOC-555HD​ is a highly specialized, ruggedized Triple Modular Redundant (TMR) Input/Output Controller​ designed for mission-critical and safety-instrumented applications, likely within the aerospace, defense, or nuclear industries. The «CCC» manufacturer is almost certainly Curtiss-Wright Controls, a leader in high-reliability embedded computing. The designation «TIOC» stands for Triple I/O Controller, and «555HD» indicates a specific high-density or high-performance variant within the product family. This unit is a sophisticated electronic assembly that provides a fault-tolerant interface between a TMR (Triple Modular Redundant) safety controller or flight computer and the physical sensors and actuators in the field. Its core function is to acquire analog and digital input data from critical field devices through three independent, parallel signal paths, perform 2-out-of-3 (2oo3) voting on the inputs, and output voted control commands to actuators, ensuring system operation even in the presence of a single channel failure.
The value of the CCC TIOC-555HD​ lies in its uncompromising fault tolerance, high reliability, and deterministic performance​ for the most demanding control environments. It is engineered to meet stringent standards such as DO-254​ for airborne hardware design assurance and DO-160​ for environmental testing. By implementing TMR architecture at the I/O level, it provides an extremely high level of safety integrity, preventing a single point of failure in the I/O subsystem from causing a hazardous event. For system architects in applications like fly-by-wire flight control, engine control (FADEC), or safety-critical industrial processes, the TIOC-555HD is a key building block that enables the design of systems with Design Assurance Level (DAL) A​ or Safety Integrity Level (SIL) 4​ requirements, where failure is not an option.

Technical Specifications

Parameter Name
Parameter Value
Product Model
CCC TIOC-555HD
Manufacturer
Curtiss-Wright Controls
Product Type
Triple Modular Redundant (TMR) Input/Output Controller
Architecture
Triple Modular Redundancy (TMR)​ with 2-out-of-3 (2oo3) voting on all critical I/O channels. Three independent, synchronized channels (A, B, C) operate in lockstep.
I/O Types & Density
High-density mix of configurable I/O. Likely includes:

  • Analog Inputs:​ High-resolution, isolated inputs for sensors (e.g., LVDT/RVDT, pressure, temperature).
  • Digital Inputs:​ For discrete status signals (e.g., switch positions).
  • Analog Outputs:​ For driving actuators (e.g., servo valves).
  • Digital Outputs:​ For solenoids, relays.
  • Discrete (Discrete) I/O:​ Often a term for high-current/voltage digital I/O.
    Communication Interface | High-speed, deterministic interfaces to the host TMR processors, typically via:
  • Dual/Redundant MIL-STD-1553​ databus.
  • ARINC 429​ channels.
  • Ethernet (AFDX/ARINC 664)​ for modern implementations.
  • Custom parallel/serial buses.
    Voting & Synchronization | Sophisticated hardware and firmware for bit-level and word-level synchronization and voting of input data and output commands between the three channels.
    Diagnostics & Built-In Test (BIT) | Extensive continuous and initiated Built-In Test (BIT). Monitors channel health, cross-channel data consistency, power supply, and internal logic. Provides detailed fault isolation and reporting.
    Form Factor | Typically a 3/4 ATR​ or full ATR​ short/long ruggedized chassis, or a VPX/CompactPCI form factor with conduction or air cooling.
    Operating Temperature | Extended military/airborne range:​ -40°C to +85°C or wider, with conduction-cooled variants for extreme environments.
    Power Supply | 28V DC (standard aircraft) or wide-range MIL-STD-704 input, with internal power conditioning and monitoring.
    Environmental | Designed and tested to meet MIL-STD-810​ for shock/vibration and MIL-STD-461​ for EMI/EMC. Compliant with RTCA/DO-160​ environmental conditions.
    Software/Config | Requires low-level hardware configuration and integration with the host TMR software. May be supported by specific board support packages (BSPs).
TIOC-555HD

Key Features and Advantages

CCC TIOC-555HD​ is distinguished by its inherent fault tolerance at the I/O layer. Its foremost advantage is providing true triple redundancy from the sensor/actuator interface inward. Unlike systems where redundancy starts at the processor, the TIOC ensures that a failure in a signal conditioner, an A/D converter, or an output driver in one channel is masked by the two healthy channels. This delivers an extremely high level of safety availability and prevents nuisance trips. The deterministic, lockstep operation​ of the three channels is critical for time-critical control loops.
Advanced diagnostics and high reliability design​ are engineered into its DNA. The module incorporates comprehensive Built-In Test (BIT)​ that can detect over 95% of potential faults. This includes monitoring for «stuck-at» faults, out-of-sync conditions, and invalid data. The ability to isolate a fault to a specific channel or component is essential for maintenance and system health management. Constructed with high-reliability (Hi-Rel) components and designed for harsh environments, it offers a long mean time between failures (MTBF), which is paramount in applications where maintenance access is limited (e.g., in-flight).
Seamless integration into safety-critical architectures​ is a key benefit. As a product from Curtiss-Wright, it is designed to work seamlessly with other TMR components (processors, communication modules) within a defined system architecture (e.g., for flight control or engine control). Its standard rugged form factors (ATR, VPX) and communication protocols (1553, ARINC 429) make it a preferred, off-the-shelf choice for aerospace integrators, reducing development risk and time compared to a custom-designed solution. In summary, the TIOC-555HD​ provides the robust, intelligent, and fault-tolerant «hands and senses» required for the most critical automated systems on earth.

Application Areas

The CCC TIOC-555HD​ is deployed in the most demanding, safety-critical control systems​ where failure could result in catastrophic consequences.
Its primary application domains are:
  • Aerospace & Defense:
    • Fly-by-Wire Flight Control Systems:​ Primary flight control actuation and surface position sensing.
    • Full Authority Digital Engine Control (FADEC):​ Interface with engine sensors (temperature, pressure, speed) and fuel metering valves.
    • Utility Management Systems:​ For landing gear, brakes, and other critical aircraft systems.
  • Industrial Safety Systems:
    • Nuclear Power Plant Protection Systems:​ Where the highest Safety Integrity Level (SIL 4) is required.
    • Rail Transportation Control:​ For safety-critical train control functions.
Essentially, it is used in any application that requires a Design Assurance Level (DAL) A​ per DO-178C/DO-254 or SIL 4​ per IEC 61508, and where a TMR architecture is mandated to achieve the necessary level of fault tolerance and reliability.

Related Products

  • TMR Processor Modules (e.g., from Curtiss-Wright):​ The triple-redundant main computers that the TIOC interfaces with.
  • MIL-STD-1553 or ARINC 829 Interface Cards:​ For integration into the vehicle data network.
  • Power Supply Modules:​ Ruggedized, redundant 28V DC or MIL-STD-704 compliant power supplies.
  • Sensor & Actuator Specific Conditioners:​ LVDT/RVDT signal conditioners, solenoid drivers, though much of this may be integrated into the TIOC.
  • System Integration & Testing Services:​ Provided by Curtiss-Wright or specialized integrators for these complex systems.
  • Airborne Chassis/Enclosures:​ ATR racks or VPX backplanes for housing the module.

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