Aircraft Undercarriage Wheel Speed Measurement Dual Processor Architecture

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Solution Overview

Problem

Traditional aircraft wheel tachometers, especially those using active sensors, are prone to reduced reliability due to sensitivity to mechanical stresses, temperature, and moisture cycles, leading to potential loss of anti-lock function when additional components fail.

Innovation Solution

A measurement device with dual processor units and measurement units for each wheel, where each processor unit powers and acquires signals from both measurement units, ensuring that a failure in one processor does not disrupt the anti-lock function, and amplifiers are used to compensate for signal differences.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If additional functions (digitizing, filtering, processing, transmitting) are added to the tachometer using electrical power supply, then the measurement capabilities and functionality are improved, but the reliability is reduced due to increased sensitivity to mechanical stresses, temperature, and moisture cycles

Engineering Contradiction:
Improvemeasurement functionalityVSAvoidtachometer reliability
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The system divides the tachometer functions into separate processor units, with each processor unit responsible for specific wheels. This segmentation isolates failures to individual processor units rather than causing complete system failure, thereby maintaining reliability while preserving enhanced measurement functionality.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Each processor unit is dedicated to specific wheels and contains localized processing capabilities. This local quality approach ensures that failures are contained locally and do not propagate throughout the entire system, maintaining overall system reliability while providing advanced measurement functions where needed.

Inventive Principle:
Principle #3Local quality

2Device complexity

If a single processor unit is used per tachometer, then the device complexity is reduced, but the reliability is reduced because a single failure disables the entire anti-lock function

Engineering Contradiction:
Improveprocessor configurationVSAvoidanti-lock function reliability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The system segments the processor functions into multiple independent processor units, each handling specific wheels. This segmentation increases reliability through functional distribution while keeping each individual processor unit relatively simple in design.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system changes the architectural parameter from a single centralized processor to multiple distributed processors. This parameter change transforms the system from vulnerable to resilient, as failures in one processor do not compromise the entire anti-lock function.

Inventive Principle:
Principle #35Parameter changes

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This configuration significantly improves the reliability of the anti-lock function by reducing the failure rate of the measurement device, effectively doubling the mean time between critical failures and ensuring continuous operation even if one processor unit fails.

Implementation Method 1

The passive sensor thus includes a coil having terminals across which a measurement voltage is induced, which voltage is representative of the speed of rotation of the wheel

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 2

Attempts have been made to improve the accuracy with which the speed of rotation of the wheel is measured and to improve the sensitivity of the measurement at low speed by using an active sensor, e.g., a Hall effect sensor

Methodology Applied
Scientific EffectHall effect: Hall Effect

Data Source

PatentUS10900989B2Device for measuring the speeds of rotation of at least two wheels of an aircraft undercarriage
Publication Date: 2021.01.26 SAFRAN LANDING SYSTEMS
  • US10900989B2 patent drawing
  • US10900989B2 patent drawing
  • US10900989B2 patent drawing

AI summary

A measurement device for measuring speeds of rotation of at least two wheels of an aircraft undercarriage includes a measurement unit and a processor unit associated with each wheel. The measurement unit of each wheel is configured to transform the speed of rotation of the wheel into an electrical magnitude. The processor unit of each wheel is configured to acquire the electrical magnitudes produced by at least two measurement units in order to transform the electrical magnitudes into digital measurement signals representative of the speeds of rotation of at least two wheels, and in order to transmit the digital measurement signals to external equipment.