Redundant Magnetic Rotary Position Sensor for Wear-Free Pilot Control
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Solution Overview
Problem
Potentiometers in aircraft pilot control units suffer from reduced endurance due to wear between the metal wiper and resistive track, leading to performance loss, increased noise, and potential loss of contact.
Innovation Solution
A contactless DC voltage rotary position sensor using a rotatable magnet and stationary PCBs with integrated circuits to sense the magnetic field, providing multiple outputs on a single shaft without the need for a metal wiper and resistive track.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If potentiometers are used for position feedback, then the electrical interface is simple and multiple outputs can be provided in a small volume, but wear and endurance are reduced due to contact between metal wiper and resistive track
Solution Approach 1:
The patent replaces the mechanical contact-based potentiometer system with a magnetic field-based sensing system. A magnet rotates with the shaft while stationary magnetic sensors on PCBs detect the magnetic field variations, eliminating the metal wiper and resistive track contact. This substitution of mechanical contact with magnetic field detection resolves the wear and endurance issue while maintaining the multiple outputs capability.
Solution Approach 2:
The patent introduces a magnetic field as an intermediary between the rotating shaft and the stationary sensors. The magnet attached to the rotating shaft creates magnetic field variations that are detected by the stationary magnetic sensors on the PCBs. This intermediary allows position feedback without direct mechanical contact, eliminating wear while transmitting rotational position information.
2Reliability
If redundant sensors are added to improve reliability, then measurement accuracy improves, but device complexity increases
Solution Approach 1:
The patent merges multiple sensing functions onto a single PCB substrate. Multiple magnetic sensors are integrated on the same PCB, allowing redundant position measurement capabilities within a compact form factor. This consolidation approach provides reliability through redundancy while minimizing the increase in device complexity by sharing common infrastructure.
Solution Approach 2:
The PCB serves multiple functions: it provides mechanical support for the magnetic sensors, electrical connections for multiple outputs, and housing integration. The magnetic sensor system itself provides both primary position feedback and redundant measurement capabilities. This multi-functionality reduces overall device complexity while maintaining reliability through redundancy.
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
The solution enhances the endurance and reliability of position sensors by eliminating wear-related issues, allowing for multiple outputs in a compact form factor suitable for aircraft pilot control units, with improved accuracy and reduced noise.
Implementation Method 1
The rotary position sensor includes a rotatable magnet creating a magnetic field and at least one of a pair of first and second magnetic field sensors
Data Source
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AI summary
A DC voltage rotary position sensor (200) is described herein comprising a shaft and magnet assembly (290) comprising a rotatable shaft (210) having a magnet (220) provided thereon, said shaft and magnet assembly (290) being rotatable about an axis of rotation X to create a magnetic field; a first printed circuit board (PCB) (230) located at a first side of said magnet (200) and on said axis of rotation X; said first PCB (230) having a first integrated circuit (IC) (250) provided thereon and being configured to sense the direction of said magnetic field as said magnet (220) rotates about said axis X to thereby determine relative movement of said sensor (200). A method of making a sensor is also described.