Aircraft Seat Control Unit with Monitored Communication Isolation

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Solution Overview

Problem

Existing aircraft seat control units lack robust security measures to prevent unauthorized access and manipulation, leading to potential safety risks and complex certification processes for software updates.

Innovation Solution

The aircraft seat control unit is designed with a separate communication circuit unit and function circuit unit, where the function circuit monitors the communication circuit for errors and manipulations, allowing for independent software operation and updates without affecting certification of the trustworthier function circuit unit.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the communication circuit unit is integrated with the function circuit unit, then device complexity is reduced, but security and reliability are compromised due to inability to independently monitor and update communication software

Engineering Contradiction:
ImprovesecurityVSAvoidstructural complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The control unit is divided into two independent circuit units: a function circuit unit for controlling aircraft seat functions and a communication circuit unit for handling external communications. This segmentation allows the communication unit to be separately monitored and updated without affecting the function unit, thereby improving security while maintaining manageable complexity through modular design.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A monitoring mechanism is introduced where the function circuit unit monitors the communication circuit unit for errors and manipulations. This intermediary monitoring relationship enables security oversight of the communication unit without requiring full integration, resolving the contradiction between security and complexity.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If software updates are implemented in the control unit, then adaptability is improved, but certification complexity increases due to potential security risks

Engineering Contradiction:
Improvesoftware update capabilityVSAvoidcertification complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The software system is segmented into separate operating programs: a first operating program on the function circuit unit and a second operating program on the communication circuit unit. The monitoring mechanism detects manipulations in the second program without requiring recertification of the first program, enabling software updates while reducing certification complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The monitoring mechanism is pre-configured to detect manipulations and trigger automatic responses. This preliminary action ensures that security measures are in place before updates occur, allowing adaptability through updates while maintaining certification compliance through pre-established monitoring protocols.

Inventive Principle:
Principle #10Preliminary action

3Reliability

If the communication circuit unit is monitored by the function circuit unit, then security is enhanced, but device complexity increases

Engineering Contradiction:
ImprovesecurityVSAvoidcontrol complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The function circuit unit performs self-monitoring of the communication circuit unit through integrated monitoring functionality. This self-service approach enhances security through continuous monitoring while avoiding the need for external monitoring systems, thereby limiting the increase in device complexity.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS20250304260A1Aircraft seat control unit
Publication Date: 2025.10.02 RECARO AIRCRAFT SEATING GMBH & CO KG
  • US20250304260A1 patent drawing
  • US20250304260A1 patent drawing

AI summary

An aircraft seat control unit for an aircraft seat has a function circuit unit, which includes at least one function circuit for controlling the aircraft seat, and has a communication circuit unit which includes at least one communication circuit and is configured for communication with at least one external control unit, wherein the communication circuit unit is realized separately from the function circuit unit, at least with respect to software technology, and the function circuit unit is configured to monitor the communication circuit unit.