Composite Rotor Sleeve for Electromechanical Machines
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Solution Overview
Problem
Electromechanical machines with traditional rotor assemblies are heavy and costly due to numerous brazing operations and flux pinch points, which increase exciter and main field current flow, leading to inefficiencies in aircraft systems.
Innovation Solution
A rotor assembly design featuring a composite sleeve made of carbon fibers, copper fibers, and epoxy resin surrounding the rotor core, which functions as both a structural support and a damper circuit to manage electromagnetic flux, reducing the need for brazing and minimizing flux pinch points.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If traditional rotor assembly with multiple damper bars and copper end-plates is used, then the damper circuit can be electrically connected, but numerous brazing operations are required making the assembly heavy and costly
Solution Approach 1:
The patent merges the damper bars and end-plates into a single integrated composite sleeve structure. The sleeve contains conductive elements (such as copper wires or conductive particles) embedded within a non-conductive matrix material, eliminating the need for separate damper bars and copper end-plates that require brazing operations. This integration reduces the number of components and assembly steps while maintaining the electrical connection function of the damper circuit.
Solution Approach 2:
The patent employs composite materials for the sleeve structure, combining conductive elements (copper wires, particles, or flakes) with a non-conductive matrix material (such as epoxy resin, plastic, or ceramic). This composite construction provides both structural support and electrical conductivity within a single component, replacing the traditional separate metal parts and reducing overall weight while maintaining functional performance.
2Reliability
If traditional rotor assembly with damper bars in slots is used, then the damper circuit can be formed, but flux pinch points are created that limit electromagnetic flux communication
Solution Approach 1:
The patent merges the damper circuit function into a continuous sleeve structure that surrounds the rotor core without creating discrete slots or interruptions. This continuous structure eliminates the flux pinch points that occur at damper bar locations in traditional designs, allowing electromagnetic flux to communicate more efficiently between the rotor and stator assemblies.
Solution Approach 2:
The composite sleeve provides a more homogeneous structure compared to the discontinuous damper bars in slots. The embedded conductive elements are distributed throughout the matrix material, creating a uniform structure that does not create localized flux interruptions or pinch points, thereby improving electromagnetic flux communication efficiency.
3Reliability
If traditional rotor assembly with multiple brazing operations is used, then the damper circuit can be assembled, but manufacturing cost increases
Solution Approach 1:
The patent merges multiple discrete components (damper bars, copper end-plates, brazing materials) into a single integrated composite sleeve. This eliminates the need for multiple brazing operations, reducing manufacturing complexity, assembly time, and associated costs while maintaining the electrical connection function of the damper circuit.
Solution Approach 2:
The patent replaces the mechanical brazing process with a composite material fabrication process. Instead of joining separate metal parts through brazing, the conductive elements are embedded within the matrix material during composite fabrication, which can be done through molding or curing processes. This substitution eliminates the need for specialized brazing equipment and operations, reducing manufacturing cost.
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
The composite sleeve design reduces the weight and cost of electromechanical machines while enhancing electromagnetic flux communication, thereby improving aircraft efficiency by minimizing flux pinch points and current flow requirements.
Implementation Method 1
One of the outer sleeve and the inner sleeve dampens electromagnetic flux generated by the rotor assembly
Implementation Method 2
The field windings generate the electromagnetic flux necessary to induce a magnetic field within a stator assembly of the electromechanical machine
Data Source
AI summary
A rotor assembly for an electromechanical machine includes a rotor core, an outer sleeve and an inner sleeve. The rotor core includes an outer diameter, and the outer sleeve is positioned about the outer diameter. The inner sleeve is positioned between the rotor core and the outer sleeve. One of the outer sleeve and the inner sleeve dampens electromagnetic flux generated by the rotor assembly.


