Nested Guide Tube Assembly for Gas Turbine Inspection
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Solution Overview
Problem
Visual inspection of internal components and fasteners within gas turbine engines is challenging due to confined spaces and complex pathways, making it difficult to access and inspect areas such as the compressor, combustion chamber, and turbine.
Innovation Solution
A multi-tube assembly comprising a rigid guide tube and a pre-shaped flexible guide tube, where the flexible guide tube is inserted through the rigid guide tube to navigate past interior components, allowing a tool, such as a borescope, to reach inaccessible areas by manipulating the flexible guide tube's shape and position.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of operation
If a rigid inspection tool is used to inspect internal components, then the tool structure is simple and durable, but the tool cannot navigate complex pathways and confined spaces within the engine
Solution Approach 1:
The patent employs a nested tube structure where a flexible guide tube is inserted through a rigid guide tube. The rigid outer tube provides structural support and protection, while the flexible inner tube can bend and navigate complex pathways. This nested configuration allows the inspection tool to access confined spaces and follow complex engine internal pathways while maintaining structural integrity and durability through the rigid outer protection.
Solution Approach 2:
The patent utilizes a flexible guide tube with a pre-formed shape that can bend and conform to the complex internal geometry of the gas turbine engine. This flexible tube allows the inspection tool to navigate around obstacles and reach inaccessible areas within the engine, solving the problem of accessing confined spaces while maintaining a relatively simple overall tool structure.
2Adaptability or versatility
If a flexible guide tube is used to navigate complex pathways, then the tool can reach inaccessible areas, but the tool becomes more complex and harder to control
Solution Approach 1:
The nested tube structure provides inherent control mechanisms where the rigid outer tube constrains and guides the flexible inner tube's movement. This configuration allows the flexible tube to reach inaccessible areas while the rigid tube maintains directional control and prevents excessive bending, thereby reducing operational complexity despite increased adaptability.
Solution Approach 2:
The flexible guide tube is pre-formed with a specific shape configuration that is predetermined to match the engine's internal pathway geometry. This pre-shaping reduces the complexity of real-time control during operation, as the tube's shape is already optimized for navigating the specific complex pathways it will encounter within the gas turbine engine.
3Adaptability or versatility
If the tool is extended to reach remote areas, then inspection coverage is improved, but the tool is more vulnerable to damage
Solution Approach 1:
The rigid outer guide tube serves as a protective sheath for the flexible inner tube and the inspection tool. This nested configuration extends inspection coverage to remote areas while the rigid outer tube provides mechanical protection against damage from engine components, debris, and environmental factors, thereby maintaining tool reliability despite extended reach.
Solution Approach 2:
The flexible guide tube acts as a protective conduit that can absorb and distribute mechanical stresses encountered during navigation through complex pathways. Its flexibility allows it to conform to engine geometry without transmitting excessive forces to the inspection tool, reducing damage risk while maintaining extended reach capability.
Data Source
AI summary
A method of servicing a portion of a gas turbine engine includes inserting a rigid guide tube into an inspection port in a shroud of the gas turbine engine. The flexible guide tube is inserted into and through the rigid guide tube. The flexible guide tube is pre-shaped such that the flexible guide tube is biased towards a predetermined shape after being inserted through the rigid guide tube. A tool is pushed through the flexible guide tube such that the distal end of the tool moves out of and away from an end of the flexible guide tube. An area of interest of the gas turbine engine is then serviced with the tool.


