Aircraft Anti-icing System Automatic Mode Switching

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Solution Overview

Problem

Existing anti-icing systems on aircraft lack the ability to automatically switch to a safe operation mode in case of a breakdown, potentially leading to reduced safety and instability during flight due to inadequate control over anti-icing devices.

Innovation Solution

An anti-icing system that includes operation mode selecting means and control means to manage anti-icing devices, allowing automatic mode operation if a breakdown is detected, and utilizing flight altitude information to switch modes, ensuring reliable control and enhanced safety.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If manual mode is selected by operation mode selecting means, then pilot's intention is prioritized, but system reliability decreases when switch breaks down

Engineering Contradiction:
Improvepilot's intention priorityVSAvoidsystem reliability
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The control means is designed to detect breakdowns in the operation mode selecting means and automatically switch to automatic mode as a pre-prepared backup mechanism. This beforehand cushioning ensures that when a manual switch breaks down, the system has already prepared an alternative control path that maintains safety without requiring pilot intervention.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Solution Approach 2:

The control means continuously monitors the operation mode selecting means for breakdowns and provides feedback to switch the operation mode from manual to automatic when a breakdown is detected. This feedback mechanism ensures the system adapts to component failures and maintains reliable operation by transitioning to a safer automatic control state.

Inventive Principle:
Principle #23Feedback

2Reliability

If automatic mode is used, then system reliability improves, but pilot's control authority decreases

Engineering Contradiction:
Improvesystem reliabilityVSAvoidpilot's control authority
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The operation mode is made dynamic rather than fixed, allowing the system to transition between manual and automatic modes based on real-time conditions. The control means can switch between modes depending on whether the operation mode selecting means is functioning properly, giving the pilot control authority when needed and automated reliability when safety is prioritized.

Inventive Principle:
Principle #15Dynamics

3Reliability

If switch breakdown is detected, then automatic mode should activate, but system complexity increases

Engineering Contradiction:
Improvesafety in emergencyVSAvoidcontrol system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The control means automatically detects breakdowns in the operation mode selecting means and switches to automatic mode without requiring external intervention or complex diagnostic procedures. The system serves itself by monitoring its own components and taking appropriate action, which simplifies the overall architecture compared to systems requiring manual backup procedures.

Inventive Principle:
Principle #25Self-service

4Ease of operation

If manual mode is maintained until predetermined altitude, then pilot's intention is respected, but safety response time decreases

Engineering Contradiction:
Improvepilot's intention priorityVSAvoidsafety response time
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The control means is pre-programmed to monitor for switch breakdowns continuously and automatically activate automatic mode when a breakdown is detected, regardless of the current operation mode or flight altitude. This preliminary action ensures that safety mechanisms are activated immediately upon detecting a failure condition, without waiting for pilot response or altitude thresholds.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS9334057B2Anti-icing system and aircraft
Publication Date: 2016.05.10 MITSUBISHI AIRCRAFT
  • US9334057B2 patent drawing
  • US9334057B2 patent drawing
  • US9334057B2 patent drawing

AI summary

Provide is an anti-icing system that can cause anti-icing devices to properly operate even if a breakdown occurs in a switch after a pilot sets the switch.An anti-icing system of the present invention that controls operations of anti-icing devices provided in an aircraft includes: operation mode selecting means that selects an operation mode of the anti-icing devices; and control means that controls the operations of the anti-icing devices according to the operation mode selected by the operation mode selecting means. The operation mode includes at least a manual mode, an automatic mode, and a stop mode, and the control means controls the operations of the anti-icing devices in the automatic mode if detecting that a breakdown occurs in the operation mode selecting means when the manual mode or the stop mode is selected by the operation mode selecting means.