Profiled Target Sensing for Lightweight Propeller Blade Pitch Measurement
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Existing propeller blade pitch sensing systems are heavy and mechanically complex, utilizing hydraulic actuation and position sensors like RVDT or LVDT, which are cumbersome and not optimized for aircraft safety and dispatchability.
Innovation Solution
A sensing system with a target portion having a profile that changes with distance along an axis, using non-translating distance sensors to determine pitch angle, allowing for a lightweight and low-complexity system that operates independently of rotational speed and provides redundancy through multiple sensors.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Measurement precision
If hydraulic actuation systems with position sensors (RVDT or LVDT) are used to control propeller blade pitch, then the blade pitch can be accurately controlled and sensed, but the system becomes heavy and mechanically complex
Solution Approach 1:
The patent replaces complex mechanical position sensors (RVDT or LVDT) with a simplified optical sensing system. A target portion with a coded pattern (e.g., reflective or absorptive regions) is coupled to the pitch actuator, and an optical sensor detects the pattern to determine pitch position. This substitution eliminates heavy mechanical components while maintaining measurement accuracy through optical detection of the coded pattern's position or orientation.
Solution Approach 2:
The patent uses a coded pattern on the target portion that encodes pitch position information. Instead of directly measuring physical displacement with complex sensors, the system captures an optical image or signal representing the coded pattern and decodes it to determine pitch angle. This copying approach converts mechanical position information into an optical signal that can be processed electronically, reducing mechanical complexity.
2Measurement precision
If traditional position sensors are used in the sensing system, then blade pitch can be measured, but the system requires calibration at aircraft level and is not optimized for safety and dispatchability
Solution Approach 1:
The sensing system is designed to be self-calibrating or self-configuring. The coded pattern on the target portion provides reference features that enable the sensor to automatically determine its own position and orientation relative to the pitch mechanism. This eliminates the need for external calibration equipment and procedures at aircraft level, allowing the system to be calibrated during manufacturing or initial setup and then operate autonomously throughout its service life.
Solution Approach 2:
The calibration and configuration of the sensing system is performed in advance during manufacturing or system assembly, rather than requiring field calibration. The coded pattern is pre-configured with known geometric features, and the sensor is pre-aligned with reference markers. This preliminary setup ensures the system is ready for immediate safe operation upon installation, optimizing dispatchability.
3Weight of moving object
If a lightweight sensing system is implemented, then system weight and complexity are reduced, but measurement reliability must be maintained for aircraft safety
Solution Approach 1:
The patent changes the measurement parameter from direct mechanical displacement to optical detection of a coded pattern. The target portion includes regions with different optical properties (reflective, absorptive, transparent) arranged in a coded pattern. The optical sensor detects these optical parameter variations to determine pitch position, enabling lightweight construction while maintaining reliability through robust optical signal detection and error-correcting code design.
Solution Approach 2:
The sensing system incorporates redundancy and error tolerance in its design. The coded pattern uses error-correcting codes or redundant encoding schemes that can tolerate some signal degradation or sensor errors. Multiple sensor elements or multiple readings can be averaged or cross-checked. This beforehand cushioning against potential failures ensures reliable operation even with lightweight, less robust components.
Data Source
Figure 1
Figure 2
Figure 3
AI summary
A sensing system and a method of sensing are disclosed. The sensing system has a sensor apparatus (140) and a target portion (124) for sensing by the sensor apparatus (140). The target portion (124) is integral with, or configured for coupling to, a component of an assembly so as to translate along an axis, and the target portion (124) has an outer surface which has a profile that changes with distance along the axis. The sensor apparatus (140) is configured for non-translating mounting adjacent the target portion (124), and has at least one distance sensor (142, 144). The method comprises sensing a distance between the distance sensor (142, 144) and the outer surface of the target portion (124), wherein the sensed distance varies as the target portion (124) translates axially, and outputting a signal in dependence on the sensed distance.