Rotor Balancing via Dynamic Pitch Adjustment

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Solution Overview

Problem

Utility-grade wind turbines face imbalanced loading issues due to mass imbalances, geometrical irregularities, and aerodynamic differences in rotor blades, leading to fatigue damage and failure of components like bedplates, nacelles, and main shaft bearings.

Innovation Solution

A method for balancing the rotor by using sensors to measure loads, accelerations, and displacements, determining pitch offset angles, and adjusting blade pitch angles to reduce bending moments, thereby balancing the rotor and minimizing imbalanced loads.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If traditional rotor balancing methods are used, then manufacturing precision can be improved, but device complexity and operational reliability remain insufficient due to inability to address dynamic imbalances during operation

Engineering Contradiction:
Improverotor balancing precisionVSAvoidcomponent reliability under dynamic loads
Core Design Contradiction:
Manufacturing precisionVSReliability

Solution Approach 1:

The system performs preliminary measurement and analysis of imbalance conditions during normal operation, then proactively adjusts blade pitch angles to correct imbalances before they cause fatigue damage or component failure

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention transitions from static manufacturing balancing to dynamic operational balancing by continuously measuring loads during rotation and adjusting blade pitches in real-time to adapt to changing operational conditions

Inventive Principle:
Principle #15Dynamics

2Object-generated harmful factors

If blade pitch angles are adjusted to balance the rotor, then imbalanced loads are reduced, but this requires complex measurement and control systems

Engineering Contradiction:
Improveimbalanced loadsVSAvoidmeasurement and control system complexity
Core Design Contradiction:
Object-generated harmful factorsVSDevice complexity

Solution Approach 1:

The invention replaces complex mechanical balancing mechanisms with a control system that uses sensors to measure loads and electronically adjusts blade pitch angles, substituting mechanical complexity with electronic control

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The system implements a closed-loop feedback mechanism where sensors continuously measure loads and accelerations, the controller processes this data to determine optimal pitch adjustments, and the pitch actuators implement corrections, creating an automatic self-regulating system

Inventive Principle:
Principle #23Feedback

3Measurement precision

If multiple sensors are used to measure loads, accelerations, and displacements, then measurement precision improves, but device complexity increases

Engineering Contradiction:
Improveload and acceleration measurement precisionVSAvoidsensor and measurement system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The sensor system is designed to perform multiple functions simultaneously - measuring loads, accelerations, and displacements with a integrated sensor array, reducing overall system complexity compared to separate measurement systems for each parameter

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The measurement system automatically captures and processes data during normal operation without requiring external intervention, and the controller self-adjusts pitch angles based on measured parameters, eliminating the need for external balancing equipment

Inventive Principle:
Principle #25Self-service

Data Source

PatentEP1870596B1Apparatus for balancing a rotor
Publication Date: 2017.02.15 GENERAL ELECTRIC CO
  • EP1870596B1 patent drawing
  • EP1870596B1 patent drawing
  • EP1870596B1 patent drawing

AI summary

A rotary machine (10) includes a rotor (18) including a hub (22), at least two rotor blades (24) coupled to the hub, and a rotor shaft (28, 30) coupled to the hub for rotation. At least one blade pitch actuator (56) is coupled to at least two rotor blades for controlling an angle of pitch of at least two rotor blades. At least one sensor (48, 50) is configured to measure at least one of a load, an acceleration, and a displacement that pertains to at least one bending moment acting on the rotor shaft. A processor (64) is coupled to at least one blade pitch actuator and coupled to at least one sensor. The processor is configured to balance the rotor by receiving (102), from at least one sensor, at least one measurement of either a load, an acceleration, or a displacement that pertains to at least one bending moment acting on said rotor shaft. Determining (104) at least one value of at least one bending moment acting on the rotor shalt based, at least in part, on the received at least one measurement and determining (106) a pitch offset angle value for at least one rotor blade that facilitates reducing the at least one bending moment acting on said rotor shaft.