Optical Bore Measurement in Aircraft Drilling for Rivet Precision
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Solution Overview
Problem
The existing manufacturing systems for producing airplane structural components face limitations in measuring bore geometry parameters, particularly in flexibility and accuracy, especially when dealing with multiple material plies and fiber composite materials, due to the use of capacitive measuring units which struggle with low resolution and material-dependent measurement accuracy.
Innovation Solution
Implementing an optical scanning system with a measuring unit comprising an interferometer arrangement, using an optical sensor element and measuring lance to point-by-point scan the bore inner surface, allowing for high in-plane resolution and flexibility, and integrating measurement cycles into the manufacturing process to adjust for geometry parameter deviations.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Measurement precision
If a capacitive measuring unit is used to measure bore geometry parameters, then the measurement can be performed with a simple device structure, but the measurement precision and flexibility are restricted
Solution Approach 1:
The patent replaces the capacitive measuring system with an optical measuring system that uses a laser beam to scan the bore inner surface. The optical system includes a laser source, optical scanner, and detector that work together to measure bore geometry parameters with high precision. This substitution of mechanical/electrical measurement with optical measurement resolves the contradiction by achieving higher measurement precision while maintaining acceptable device complexity through the use of non-contact optical fields.
Solution Approach 2:
The patent introduces an optical intermediary system consisting of optical scanners and laser beams that mediate between the measuring device and the bore surface. The optical fields act as intermediaries to transfer measurement information from the bore geometry to the detector without direct physical contact, thereby achieving high measurement precision while avoiding the complexity of direct capacitive sensing arrangements.
2Adaptability or versatility
If a capacitive measuring probe with fixed measurement portions is used, then the device structure is simplified, but the adaptability to different measurement positions and configurations is restricted
Solution Approach 1:
The patent employs dynamic optical scanning where the laser beam is swept across the bore inner surface using optical scanners. The measurement system transitions from static fixed portions to dynamic scanning that can adapt to any measurement position and configuration. The optical beam can be directed to any location within the bore by controlling the optical scanners, providing unlimited adaptability without requiring physical reconfiguration of the measuring probe structure.
Solution Approach 2:
The optical measuring system serves multiple measurement functions through a single unified device. The same laser source and optical scanner can measure various bore geometry parameters including diameter, roundness, ovality, and surface profile by simply changing the scanning pattern and detector positioning. This multi-functionality achieves high adaptability while avoiding the need for multiple specialized probes or complex reconfigurable structures.
3Measurement precision
If point-by-point optical scanning is performed with high in-plane resolution, then the measurement precision is improved, but the measurement cycle time increases
Solution Approach 1:
The patent implements continuous optical scanning where the laser beam continuously sweeps across the bore inner surface without interruption. The optical scanners operate at high frequencies to maintain continuous measurement data acquisition, ensuring that high in-plane resolution is achieved through dense sampling while minimizing idle time between measurements. This continuous action maintains high measurement precision while optimizing the measurement cycle time.
Solution Approach 2:
The patent uses periodic scanning patterns where the optical beam systematically traverses the bore surface in repeated cycles. The scanning frequency and pattern are optimized to capture sufficient measurement points for high in-plane resolution while maintaining an efficient rhythm that minimizes total measurement time. The periodic nature of the scanning allows for predictable cycle times while achieving the required measurement precision through adequate sampling density.
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 solution enables accurate and flexible measurement of geometry parameters across various material combinations, improving measurement resolution and allowing for real-time adjustments during the manufacturing process, reducing cycle time and enhancing the precision of rivet connections in airplane structural components.
Implementation Method 1
point-by-point, optical scanning of the bore inner surface... provided that the respective material surface ensures a sufficient reflection of the optical measurement beam
Implementation Method 2
the measuring unit is an interferometer arrangement in which the respective distance is ascertained with the aid of light interference
Data Source
AI summary
A manufacturing system for producing airplane structural components, including a drilling unit for producing bores in a material assembly made of at least two material plies for the purposes of inserting fastening elements and having a measuring unit for ascertaining geometry parameters for a previously produced bore. The measuring unit includes measuring electronics with an optical sensor element, a measuring optical unit and a measuring lance. The measuring unit produces an optical measurement beam that emerges from the measuring lance via the measuring optical unit and that is incident on a measurement point on the respective bore inner surface. A measurement movement between measuring lance and material assembly is provided in a measurement cycle and the measuring unit cyclically ascertains distance values to various measurement points at a scanning rate during the measurement movement and ascertains at least one geometry parameter for the respective bore from the distance values.


