Borescope Fluorescence and In-Situ Marking for Turbine Inspection
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Solution Overview
Problem
Current borescope methods and systems fail to differentiate between substances in inaccessible areas and do not allow in-situ marking of flaws with high-temperature-resistant paint in turbine engines.
Innovation Solution
A borescope system that uses UV light to excite substances for fluorescence capture and identification, combined with a pressurized air system to dispense marking fluid like thermal paint for flaw marking.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of operation
If conventional borescope methods are used for visual inspection, then accessibility to target areas is improved, but the ability to differentiate between different substances is lost
Solution Approach 1:
The patent introduces fluorescence spectroscopy as an intermediary measurement technique. The borescope delivers excitation light to the target substance and captures the emitted fluorescence spectrum, which serves as a unique identifier for different substances. This intermediary spectral measurement enables substance differentiation without requiring physical access or disassembly.
Solution Approach 2:
The patent replaces mechanical visual inspection with optical spectroscopic measurement. Instead of relying on human visual differentiation of substances through a borescope camera, the system uses fluorescence excitation and emission spectroscopy to automatically identify substances based on their spectral fingerprints, substituting mechanical observation with optical analysis.
2Measurement precision
If engine disassembly is performed to access and mark flaws, then flaw identification is improved, but time consumption and cost increase
Solution Approach 1:
The patent performs flaw marking in-situ during the borescope inspection, before engine disassembly. The system delivers marking fluid through the borescope to the identified flaw location and cures it with UV light, creating a permanent visual indicator that remains after disassembly. This preliminary action eliminates the need to reassemble and disassemble the engine solely for flaw marking purposes.
Solution Approach 2:
The patent integrates multiple functions into a single borescope system: visual inspection, fluorescence spectroscopy for substance identification, and in-situ flaw marking with UV-curable paint. This multi-functional approach consolidates what would traditionally require separate operations (inspection, analysis, and marking) into one unified process, eliminating redundant disassembly and reassembly cycles.
3Illumination intensity
If standard paint is used for flaw marking, then marking visibility is improved, but high-temperature resistance is lost
Solution Approach 1:
The patent changes the chemical and physical parameters of the marking paint to withstand high-temperature environments. Instead of using standard organic paints that would degrade, the system employs inorganic or heat-resistant formulations that maintain their visual properties and adhesion at turbine operating temperatures, while still being curable via UV initiation at the application stage.
Solution Approach 2:
The patent applies heat-resistant properties locally to the marking paint at the flaw location, while the rest of the engine components maintain their original properties. The UV-curable marking paint is applied only to the specific flaw area identified during inspection, providing localized high-temperature resistance exactly where needed for post-disassembly identification.
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
Enables substance identification and in-situ flaw marking in hard-to-reach locations, facilitating subsequent inspections by providing a durable visual indicator.
Implementation Method 1
exposing a substance in the cavity to excitation light of various wavelengths, in particular UV light, by means of the borescope; capturing a fluorescence of the excited substance by means of the borescope
Data Source
AI summary
The invention concerns a method for identifying a substance in a cavity of an apparatus, in particular in a cavity of a turbine engine or turbo machinery, comprising steps of introducing a probe tip of a borescope into the cavity; exposing a substance in the cavity to excitation light by means of the borescope; capturing a fluorescence of the excited substance by means of the borescope; and identifying the substance. The invention further concerns a borescope for identifying a substance in a cavity of an apparatus.


