Aircraft Ground Spoiler Drive System Wheel Lock Detection

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Solution Overview

Problem

Existing systems for automatically deploying aircraft ground spoilers fail to deploy them reliably when the aircraft's wheels are locked, particularly on slippery surfaces, which can prevent effective reduction of lift during landing.

Innovation Solution

A drive system that includes a wheel speed detecting part, an air speed detecting part, and a control unit that automatically deploys the ground spoiler based on predetermined wheel and air reference speeds, ensuring deployment even if the wheels are locked, and allows for delayed deployment of multiple spoilers to manage pitching moments and load distribution.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the ground spoiler is deployed based on wheel speed detection, then the deployment is simple and reliable under normal conditions, but the system fails to deploy when the wheel is locked on slippery surfaces

Engineering Contradiction:
Improveground spoiler deployment reliabilityVSAvoidcontrol system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system changes the detection parameter from wheel speed to air speed when wheel lock is detected. By monitoring air speed instead of wheel speed, the system can reliably detect landing conditions even when the wheel is locked, ensuring the ground spoiler deploys correctly without requiring complex additional sensors or mechanisms.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The system uses feedback from both wheel speed sensors and air speed sensors to determine deployment conditions. When wheel speed falls below the threshold (indicating potential lock), the system cross-checks with air speed data to confirm landing conditions and triggers deployment accordingly, improving reliability through multi-parameter verification.

Inventive Principle:
Principle #23Feedback

2Reliability

If all ground spoilers are deployed simultaneously, then the lift reduction is maximized, but an excessive pitching moment loads the nose gear excessively

Engineering Contradiction:
Improvelift reduction effectivenessVSAvoidnose gear load capacity
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The system segments the ground spoiler deployment into sequential stages rather than simultaneous activation. Multiple ground spoilers are deployed at different time intervals, with later spoilers activated after a predetermined delay following the first spoiler deployment. This segmentation distributes the pitching moment over time, preventing excessive instantaneous load on the nose gear while maintaining effective lift reduction.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS9630705B2Drive system for ground spoiler, and aircraft
Publication Date: 2017.04.25 MITSUBISHI HEAVY IND LTD
  • US9630705B2 patent drawing
  • US9630705B2 patent drawing
  • US9630705B2 patent drawing

AI summary

The present invention provides a drive system which can automatically deploy a ground spoiler even when a wheel is locked. A drive system for a ground spoiler deploys closed ground spoilers 4A to 4D when a wheel speed VW exceeds a wheel reference speed VW1 or when an air speed VB exceeds an air reference speed VB1 after a main gear 6 touches down. The system may also close the deployed ground spoilers 4A to 4D when the wheel speed VW is smaller than a wheel reference speed VW2 or when the air speed VB is smaller than an air reference speed VB2.