Permanent Magnet Rotor Section Clocking for Shaft Twist Compensation

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Solution Overview

Problem

Permanent-magnet motors in ESP systems face inefficiencies due to shaft twisting, which misaligns rotor sections, leading to reduced torque and power output, and existing solutions are complex and costly to manufacture and assemble.

Innovation Solution

The use of identically configured rotor sections with static keyways that allow for predetermined angular orientations, enabling each rotor section to be positioned in multiple circumferential positions relative to the motor shaft, thereby mitigating misalignment during operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If rotor sections are aligned when the motor is at rest, then assembly is simple, but shaft twisting causes misalignment during operation reducing torque and efficiency

Engineering Contradiction:
Improveassembly simplicityVSAvoidoperational alignment
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The rotor sections are pre-positioned at specific angular offsets during assembly so that when the shaft twists under operational torque, the magnets realign with the stator fields. This preliminary angular positioning compensates for the expected shaft deformation, maintaining synchronization between rotor magnets and stator magnetic fields during operation.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention changes the angular parameter (circumferential position) of rotor sections relative to each other. By offsetting rotor sections by specific angles (e.g., 30 degrees for four-section rotors), the system compensates for shaft twist, transforming the static alignment parameter into a dynamically compensated configuration that maintains operational efficiency.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If mechanisms are used to clock individual rotor sections, then misalignment is reduced, but device complexity and manufacturing cost increase

Engineering Contradiction:
Improvealignment maintenanceVSAvoidclocking mechanism complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Instead of using complex adjustable clocking mechanisms, the invention pre-positions rotor sections at fixed angular offsets during manufacturing. This eliminates the need for complex adjustment mechanisms while achieving the same alignment compensation effect, simplifying both the device structure and assembly process.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention uses identical rotor section designs with standardized mounting features, allowing mass production of interchangeable components. Each rotor section is a copy of the others, simplifying manufacturing and assembly while maintaining the angular offset configuration needed for compensation.

Inventive Principle:
Principle #26Copying

3Loss of energy

If rotor sections are offset to compensate for shaft twist, then torque efficiency improves, but assembly precision requirements increase

Engineering Contradiction:
Improvetorque loss reductionVSAvoidangular positioning precision
Core Design Contradiction:
Loss of energyVSManufacturing precision

Solution Approach 1:

The invention establishes specific angular parameter values for rotor section offsets (e.g., 30 degrees for four-section rotors, 45 degrees for two-section rotors). These standardized parameter values simplify the manufacturing process by providing clear target positions, reducing the actual precision burden while maintaining compensation effectiveness.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The invention applies different angular offset parameters to different rotor sections based on their position in the stack. Each rotor section has a specific local angular configuration optimized for its position, allowing precision to be managed locally at each section rather than requiring high precision across the entire assembly process.

Inventive Principle:
Principle #3Local quality

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 simplifies the manufacturing and assembly process while effectively reducing torque losses by allowing rotor sections to maintain alignment, resulting in improved efficiency and practical implementation.

Implementation Method 1

When the coils are energized, the windings generate magnetic fields that interact with the magnets of the rotor sections

Methodology Applied
Scientific EffectMagnetic field interaction: Magnetic Field

Implementation Method 2

the windings generate magnetic fields that interact with the magnets of the rotor sections. The power provided to the stator windings is controlled to cause the magnetic fields of the stator to drive the rotor sections to rotate

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 3

each rotor section in the motor develops torque which is applied to the shaft

Methodology Applied
Scientific EffectTorque transmission: Torque

Implementation Method 4

Because the shaft is long and not completely rigid, this causes the shaft to twist

Methodology Applied
Scientific EffectElastic deformation: Elasticity

Data Source

PatentUS11843285B2Systems and methods for constructing efficient permanent magnet motors
Publication Date: 2023.12.12 BAKER HUGHES OILFIELD OPERATIONS LLC
  • US11843285B2 patent drawing
  • US11843285B2 patent drawing
  • US11843285B2 patent drawing

AI summary

Systems and methods for constructing a motor having a stator, and a plurality of rotor sections secured to a shaft which is positioned to rotate within a bore of the stator. Each rotor section has permanent magnets forming corresponding magnetic poles. Each rotor section has first and second inwardly facing keyways which are identically positioned in each rotor section and are configured to enable each rotor section to be alternately positioned in at least three distinct circumferential orientations with respect to a key of the shaft. A first subset of the rotor sections is secured to the shaft in a first one of the circumferential orientations, a second subset of the rotor sections is secured to the shaft in a second one of the circumferential orientations, and a third subset of the rotor sections is secured to the shaft in a third one of the circumferential orientations.