AMR Sensor Flap Measurement for Rotor Hub
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Solution Overview
Problem
Rotor-hub flapping measurement systems in VTOL rotary aircraft face challenges with existing rotary-variable-differential transducer (RVDT) sensors due to size, weight, cost, complexity, and sensitivity to temperature and mechanical vibration.
Innovation Solution
The implementation of anisotropic magneto-resistive (AMR) sensor systems, coupled with a flap-linkage arm, to measure rotor-hub flapping by detecting movement relative to the main-rotor axis, utilizing multiple sensor arrangements for robustness and error identification.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Measurement precision
If RVDT sensors are used for rotor-hub flapping measurement, then measurement capability is achieved, but size, weight, cost, and device complexity increase
Solution Approach 1:
The patent replaces the mechanical RVDT sensor system with an AMR sensor system that uses magnetic field detection instead of mechanical components. The AMR sensor detects changes in magnetic field orientation caused by flap-linkage arm movement, eliminating complex mechanical electronics while maintaining measurement capability.
Solution Approach 2:
The patent changes the measurement parameter from direct mechanical displacement (RVDT) to magnetic field orientation changes (AMR). By attaching a magnet to the flap-linkage arm and using an AMR sensor to detect its orientation, the system measures flapping through magnetic parameter changes rather than mechanical parameter changes.
2Measurement precision
If RVDT sensors are used for rotor-hub flapping measurement, then measurement capability is achieved, but size and weight increase
Solution Approach 1:
The patent replaces the heavy mechanical RVDT sensor assembly with a compact AMR sensor and magnet combination. The AMR sensor is a solid-state device with no moving parts, significantly reducing weight while maintaining measurement functionality through magnetic field detection.
Solution Approach 2:
The patent extracts the essential measurement function from the bulky RVDT mechanism and implements it through a minimalistic AMR sensor-magnet system. Only the critical magnetic field detection components are retained, eliminating unnecessary mechanical weight.
3Measurement precision
If RVDT sensors are used for rotor-hub flapping measurement, then measurement capability is achieved, but sensitivity to temperature and mechanical vibration increases
Solution Approach 1:
The patent replaces the mechanically-sensitive RVDT system with an AMR sensor system that is inherently more resistant to mechanical vibration. The solid-state AMR sensor has no moving parts that can be affected by vibration, and magnetic field detection is less sensitive to temperature variations than mechanical components.
Solution Approach 2:
The patent introduces a magnet as an intermediary between the flap-linkage arm movement and the sensor detection. This magnetic field mediator transmits movement information to the AMR sensor without requiring direct mechanical contact, reducing sensitivity to mechanical disturbances and temperature effects.
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 AMR sensor system provides improved sensitivity and reduced variation in measurement, offering a more reliable and less complex alternative to RVDT systems, with enhanced robustness through multiple sensor configurations and error detection capabilities.
Implementation Method 1
a magneto-resistive sensor system rotatably coupled to a second end of the flap-linkage arm and responsive to movement of the flap-linkage arm
Data Source
AI summary
A rotor-hub flap-measurement system includes a rotor hub operable to flap relative to a main-rotor axis, a flap-linkage arm, a first end of the flap-linkage arm rotatably coupled to the rotor hub, the flap-linkage arm responsive to flapping of the rotor hub, and a magneto-resistive sensor system rotatably coupled to a second end of the flap-linkage arm and responsive to movement of the flap-linkage arm.


