Avionics RF Communications System with Integrated Multi-Channel Processing

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Solution Overview

Problem

Current RF avionics communications systems require multiple receivers and transmitters, increasing equipment costs and aircrew workload, and are inefficient in prioritizing and processing multiple channels, particularly during critical phases of flight.

Innovation Solution

A combined COMM and NAV/COMM system that uses a single receiver to simultaneously process and prioritize multiple channels, enabling voice-to-text conversions and automatic channel management to reduce distractions and optimize communication.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If multiple receivers and transmitters are used to monitor multiple communication channels, then communication coverage and reliability are improved, but equipment cost and device complexity increase

Engineering Contradiction:
Improvecommunication reliabilityVSAvoidavionics system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent combines multiple communication receivers into a single integrated receiver unit that can simultaneously process multiple frequencies and channels. This merging approach maintains the ability to monitor multiple communication channels while reducing the total number of separate receiver components, thereby lowering equipment cost and simplifying the avionics system architecture.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The integrated receiver is designed with multi-functional capabilities to handle various communication protocols and frequencies through software configuration rather than requiring separate hardware for each function. This universality allows a single receiver to perform the work of multiple specialized receivers, reducing device complexity while maintaining comprehensive communication coverage.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Adaptability or versatility

If multiple transceivers are installed to handle navigation and communication simultaneously, then functional capability is improved, but equipment cost and panel space increase

Engineering Contradiction:
ImproveNAV/COMM functionalityVSAvoidavionics panel complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent merges NAV/COMM and COMM transceiver functions into a single integrated unit that can operate both navigation and communication protocols simultaneously. This consolidation eliminates the need for separate panel mounts and reduces the overall number of components required, thereby maintaining full functional capability while reducing equipment cost and panel space requirements.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The integrated transceiver employs a universal design that allows it to switch between and simultaneously handle multiple functions including navigation, communication, and monitoring through software control. This multi-functionality replaces what would traditionally require multiple specialized devices, reducing avionics panel complexity while preserving all necessary operational capabilities.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Loss of information

If aircrew manually monitor multiple communication channels, then communication awareness is improved, but aircrew workload and distraction increase

Engineering Contradiction:
Improvecommunication information awarenessVSAvoidaircrew operational burden
Core Design Contradiction:
Loss of informationVSEase of operation

Solution Approach 1:

The system implements automatic channel monitoring and prioritization features that enable the avionics system to independently manage multiple communication channels without requiring continuous manual intervention from aircrew. The system automatically scans, identifies, and prioritizes relevant communications based on pre-set criteria, freeing aircrew from the burden of manually monitoring each channel while maintaining comprehensive communication awareness.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system provides automated feedback to aircrew by selectively presenting only the most relevant and high-priority communications from multiple monitored channels. This feedback mechanism filters and prioritizes information based on communication type, urgency, and operational context, allowing aircrew to maintain awareness of multiple channels without being overwhelmed by the full volume of raw communication data.

Inventive Principle:
Principle #23Feedback

4Reliability

If traditional avionics systems are used during critical phases of flight, then operational procedures are maintained, but aircrew distraction and workload increase

Engineering Contradiction:
Improveoperational safetyVSAvoidaircrew workload during critical phases
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system dynamically adjusts its monitoring and alerting behavior based on the aircraft's flight phase. During critical phases such as takeoff, landing, and approach, the system automatically modifies its operation to reduce non-essential alerts and focus only on the most critical communications, thereby maintaining operational safety while significantly reducing aircrew distraction and workload during these sensitive periods.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS11018754B2RF communications system and method
Publication Date: 2021.05.25 ONTIC ENG & MFG
  • US11018754B2 patent drawing
  • US11018754B2 patent drawing
  • US11018754B2 patent drawing

AI summary

An RF communications (COMM) system includes a COMM antenna connected to a signal processing unit including a multi-channel analog navigation/communications (NAV/COMM) transceiver and an analog COMM transmitter. The system is configured for switching between the transceiver and the transmitter, based on preprogrammed parameters including prioritizing signals based on keywords, system location and other parameters. An aircraft application is disclosed. A global navigation satellite subsystem (GNSS) subsystem can be connected to the signal processing unit for locating the telecommunications system. A method includes the steps of providing an RF communications system for aircraft and other applications.