Turbomachine Diffuser-Rectifier Assembly Using Sheet Metal Brazing
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Solution Overview
Problem
The manufacturing of radial diffusers and cylindrical rectifiers for turbomachines is challenging due to high scrap rates and limited supplier capabilities, resulting in high costs and supply issues, primarily because of the complexity and material requirements for machining thin blades and flanges.
Innovation Solution
A diffuser-rectifier assembly using sheet metal for annular flanges and cylindrical shrouds with radially oriented vanes, where the blades are soldered and brazed into openings, simplifying the manufacturing process and reducing material needs, and employing laser cutting and electrochemical machining for precise blade integration.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of manufacture
If traditional machining methods (cutting in the mass, foundry, mechanical welding) are used to manufacture diffuser and rectifier components, then structural strength and reliability are maintained, but manufacturing complexity and cost increase significantly
Solution Approach 1:
The diffuser and rectifier are divided into separate modular components: the diffuser body with its own blades, and the rectifier with separate vanes. Each component can be manufactured independently using sheet metal forming and joining techniques, allowing parallel production and simplifying the overall manufacturing process while maintaining structural integrity through designed connection interfaces.
Solution Approach 2:
Traditional mechanical machining and welding processes are replaced with sheet metal forming, laser cutting, and brazing technologies. This substitution enables more efficient manufacturing of thin-walled components with complex geometries, reducing both manufacturing complexity and cost while maintaining the required mechanical strength and reliability of the components.
2Quantity of substance
If sheet metal is used for diffuser flanges and rectifier shells, then manufacturing cost and material usage are reduced, but structural strength may be compromised
Solution Approach 1:
The invention employs thin sheet metal flanges and shells for the diffuser and rectifier components. These thin-walled structures are designed with optimized geometries and reinforcement features that maintain sufficient structural strength and rigidity while dramatically reducing material consumption and manufacturing cost compared to traditional thick-walled machined components.
Solution Approach 2:
The assembly combines sheet metal components with brazed joints to create a composite structure. The sheet metal provides the lightweight, cost-effective housing and structural framework, while the brazed connections provide strong, rigid joints that maintain overall structural integrity. This composite approach balances material efficiency with mechanical strength requirements.
3Productivity
If blades and vanes are brazed into openings in sheet metal flanges, then manufacturing efficiency and cost are improved, but precision and reliability of joints become critical
Solution Approach 1:
The blades and vanes are designed with pre-formed attachment features (such as tabs or engagement structures) that align with corresponding openings in the sheet metal flanges before brazing. This preliminary positioning ensures precise alignment and consistent joint quality, reducing the precision requirements during the actual brazing operation while maintaining high manufacturing efficiency and reliability.
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 significantly reduces manufacturing complexity and costs by at least 30% while ensuring mechanical strength and simplifying the production process, overcoming the limitations of traditional machining methods.
Implementation Method 1
the openings in the sheets are formed by laser cutting
Implementation Method 2
substantially radial vanes fixed by soldering to the cylindrical shrouds
Implementation Method 3
the ends of the blades are engaged and brazed in the openings which are formed in the flanges of the diffuser
Implementation Method 4
The diffuser vanes and those of the stator can be produced by ECM electrochemical machining
Data Source
Figure 1
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AI summary
Diffuser-rectifier assembly (10) for aircraft turbojet or turboprop, the diffuser (12) comprising annular flanges (22, 24) connected by vanes (26) and the rectifier (14) comprising cylindrical ferrules (28, 30) connected by vanes (32), the annular flanges and the cylindrical ferrules being formed of sheets to which the vanes (26, 32) are assembled by brazing.