Superconducting Winding Support Loops for Rotor Thermal Isolation

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Solution Overview

Problem

High-temperature superconducting rotor windings in electromotive machines are prone to mechanical stress, strain, and thermal challenges due to bending, torque, and over-speed conditions, leading to potential degradation and heat transfer issues that affect their structural integrity and efficiency.

Innovation Solution

A winding support structure comprising elongated loops made from high-tensile, low-thermal conductivity materials, such as fiber-reinforced polymers, provides radial and tangential support while minimizing heat transfer from the warm rotor core to the superconducting windings, using a cradle and pedestal assembly with a cryogenic transfer system to maintain the windings at critical temperatures.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If HTS rotor windings are used to increase output and efficiency, then electrical resistance is reduced to virtually zero, but the windings become sensitive to mechanical bending and tensile stresses that can cause premature degradation and winding failure

Engineering Contradiction:
Improveelectrical resistanceVSAvoidwinding integrity
Core Design Contradiction:
Loss of energyVSReliability

Solution Approach 1:

The support structure is divided into multiple functional components: a cradle for holding the winding, elongated loops for mechanical support, and a pedestal for positioning. This segmentation allows each component to be optimized for its specific function while collectively providing comprehensive protection against mechanical stresses

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The support structure utilizes composite materials with high tensile strength and appropriate mechanical properties to withstand bending and tensile stresses. The cradle, loops, and pedestal are constructed from materials engineered to provide both structural integrity and stress distribution, protecting the HTS windings from premature degradation

Inventive Principle:
Principle #40Composite materials

2Temperature

If coolant flow paths are disposed adjacent to the windings to maintain superconducting temperature, then the windings remain at or below critical temperature, but thermal isolation from the warm rotor becomes challenging

Engineering Contradiction:
Improvewinding temperatureVSAvoidthermal isolation structure
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The cradle and pedestal serve as thermal intermediary components between the warm rotor core and the cryogenically-cooled HTS windings. These structures are positioned to provide mechanical support while minimizing direct thermal conduction paths, allowing thermal isolation without requiring complex multi-layer insulation systems

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The support structure utilizes the radial dimension of the rotor to establish thermal isolation. By positioning the cradle and loops in the radial space between the rotor core and windings, the design creates thermal barriers without adding axial or tangential complexity to the cooling system

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Strength

If the support structure provides adequate mechanical support against static and dynamic loads, then winding structural integrity is maintained, but the complexity of withstanding over-speed and fault condition forces increases

Engineering Contradiction:
Improvesupport structure strengthVSAvoidsupport system complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The elongated loops are configured to provide counterbalancing support forces against centrifugal loads during over-speed conditions and fault conditions. The loop geometry and positioning create mechanical leverage that distributes dynamic forces away from the windings, reducing the complexity of requiring overly robust support structures

Inventive Principle:
Principle #8Anti-weight (Counterweight)

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 support structure effectively withstands mechanical and thermal stresses, reducing the risk of premature degradation and heat transfer, thereby enhancing the operational stability and efficiency of high-temperature superconducting electromotive machines.

Implementation Method 1

elongated loops made from high-tensile, low-thermal conductivity materials, such as fiber-reinforced polymers, provides radial and tangential support while minimizing heat transfer from the warm rotor core to the superconducting windings

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Implementation Method 2

using a cradle and pedestal assembly with a cryogenic transfer system to maintain the windings at critical temperatures

Methodology Applied
Scientific EffectCryogenic cooling: Cryogenics

Implementation Method 3

superconducting rotor windings with virtually no electrical resistance

Methodology Applied
Scientific EffectSuperconductivity: Superconductivity

Data Source

PatentUS9293959B2Apparatus to support superconducting windings in a rotor of an electomotive machine
Publication Date: 2016.03.22 SIEMENS ENERGY INC
  • US9293959B2 patent drawing
  • US9293959B2 patent drawing
  • US9293959B2 patent drawing

AI summary

An apparatus (structure) is provided to support a superconductor winding (61) of an electromotive machine. One or more elongated loops (74) and appropriate support structure (120) may be arranged to provide radial and tangential support to the superconducting winding (61). The elongated loops may be made of a material substantially resistant to heat flow. An axially-extending base assembly (100) may be arranged to anchor loops (74) with respect to the rotor core at a proximate end (76) of the elongated loops. A cradle (80) may be configured to define a recess (82) to receive the superconductor winding and to support the elongated loops at a distal end (78) of the loops.