Remote redundancy system for aircraft on-board equipment

RU2865427C1Active Publication Date: 2026-07-02МИРОНОВ СЕМЁН АНАТОЛЬЕВИЧ
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Patent Information

Authority / Receiving Office
RU · RU
Patent Type
Patents
Current Assignee / Owner
Filing Date
2025-12-17
Publication Date
2026-07-02

AI Technical Summary

Technical Problem

Existing aircraft control systems lack remote backup capabilities that can replace failed onboard equipment, leading to potential loss of functionality due to onboard system failures, and do not provide seamless redundancy or intelligent data flow management.

Method used

A remote onboard equipment backup system comprising a communication device, control device, and redundant computing resource that processes input data from the aircraft, synchronizes states, and seamlessly switches to perform the functions of failed onboard equipment elements, utilizing adaptive control and machine learning for proactive redundancy.

Benefits of technology

Enhances aircraft survivability and reliability by providing fault-tolerant, geographically distributed redundancy, reducing weight and cost, and ensuring continuous critical system operation.

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Abstract

FIELD: aviation technology.SUBSTANCE: invention relates to the systems for ensuring the reliability of aircraft, in particular to systems for redundant on-board equipment (OE) using computing resources spatially separated from the redundant OE of the aircraft. A remote backup system for on-board equipment of an aircraft comprising a communication device comprises a device for controlling the communication device, and at least one redundancy computing resource. The system is configured to exchange data with the aircraft's onboard equipment via a wireless communication channel and control the operation of the redundancy computing resource. The computing resource is configured to perform the functions of at least one element and / or system of the on-board equipment of the aircraft by processing input data received by the communication device from on board the aircraft and transmitted through the control device.EFFECT: increased survivability and reliability of aircraft is ensured by creating a distributed fault-tolerant redundancy system with the possibility of proactive control, and a reduction in the weight of the aircraft's onboard equipment.15 cl, 4 dwg
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Citation Information

Patent Citations

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