Additive Turbulator Formation on Turbomachine Surfaces
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Existing methods for forming turbulators on turbomachine surfaces often involve subtractive processes that result in waste and limited geometrical possibilities, requiring significant time and resources.
Innovation Solution
A method of depositing material onto the turbomachine surface to form turbulators, allowing for the creation of varied geometries and reducing manufacturing time by adding material, rather than removing it, using techniques like MIG welding to form turbulators on compressor, turbine, and combustor surfaces.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Manufacturing precision
If subtractive processes are used to form turbulators, then manufacturing precision can be achieved, but material waste increases and manufacturing time extends
Solution Approach 1:
The patent inverts the traditional subtractive approach by using additive build-up welding to form turbulators. Instead of removing material to create turbulator geometries, the process deposits weld material (such as austenitic or nickel-based alloys) onto the base metal surface to build up the desired turbulator shapes, thereby eliminating material waste while maintaining manufacturing precision through controlled deposition
Solution Approach 2:
The patent changes the fundamental parameter of material removal to material addition. By controlling deposition parameters (weld current, travel speed, deposition rate) and using automated welding robots with precise positioning systems, the method achieves accurate turbulator geometries through additive processes, transforming the manufacturing paradigm from subtractive to additive while reducing waste
2Ease of manufacture
If subtractive processes are used to form turbulators, then existing manufacturing methods can be maintained, but manufacturing time increases
Solution Approach 1:
The patent implements preliminary action by pre-programming the welding robot paths and parameters before production. The automated build-up welding process uses pre-configured deposition patterns and parameters, allowing rapid formation of turbulators without the time-consuming setup and execution required by subtractive methods, thereby increasing manufacturing speed while maintaining process simplicity
Solution Approach 2:
The patent replaces traditional mechanical subtractive manufacturing systems with automated welding robots that perform additive build-up welding. This substitution eliminates the need for complex machining operations, tool changes, and manual interventions, streamlining the manufacturing process and significantly reducing production time through automated, continuous deposition
3Adaptability or versatility
If diverse turbulator geometries are created, then flow characteristics are enhanced, but manufacturing complexity increases
Solution Approach 1:
The patent introduces dynamics by enabling real-time adjustment of welding parameters and robot motion paths during the build-up process. The automated system can dynamically modify deposition rates, travel speeds, and layer configurations to create various turbulator geometries (such as ribs, protrusions, or complex three-dimensional shapes) without requiring different tooling or fixtures, thereby achieving geometry versatility while maintaining manufacturing simplicity
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 approach reduces waste and manufacturing time while enabling the creation of turbulators with diverse geometries and heat transfer characteristics, enhancing flow and operational characteristics of turbomachines.
Implementation Method 1
A method of depositing material onto the turbomachine surface to form turbulators... using techniques like MIG welding
Data Source
Figure 1
Figure 2~6
AI summary
A method of forming a plurality of turbulators on a turbomachine surface (50) includes depositing a first portion of material (90) on the turbomachine surface (50) forming a first portion of the plurality of turbulators, adding additional material (94) to the first portion, and establishing a desired dimension of the plurality of turbulators.