Blade Controller Redundancy Management for Rotor Systems

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Solution Overview

Problem

Individual blade control (IBC) rotor systems face catastrophic failure due to lack of redundancy management, leading to potential loss of blade command position and system instability, as traditional control systems are not fully integrated with IBC, resulting in redundant and costly configurations.

Innovation Solution

A redundancy management method and system for IBC rotor systems, involving a control computer and blade controllers, where each blade controller queries and transmits position information, determining a lead blade for historical position validation and smoothing commands, ensuring data transfer through a slip ring between stationary and rotating frames, allowing for graceful degradation in case of communication failures.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional control systems are left intact as a safety backup for IBC, then system safety is improved, but device complexity and cost increase

Engineering Contradiction:
Improvesystem safetyVSAvoidredundant configuration
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent merges the traditional control system with the IBC system by integrating the blade position command logic into a unified control architecture. The control computer executes both traditional collective pitch control and IBC-specific blade position commands, eliminating the need for separate redundant systems while maintaining safety through the validated position command determination process.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The control system performs self-validation of blade position commands through the determination of valid positions based on lead blade positions and historical data. This self-service mechanism allows the system to detect and correct potential failures internally without requiring external redundant backup systems, reducing overall system complexity while maintaining reliability.

Inventive Principle:
Principle #25Self-service

2Reliability

If redundancy management is implemented in IBC rotor systems, then system reliability is improved, but device complexity increases

Engineering Contradiction:
Improvesystem reliabilityVSAvoidcontrol system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The control computer determines valid blade position commands in advance by referencing lead blade positions and historical data before executing control actions. This preliminary validation process prevents catastrophic failures by ensuring command validity ahead of time, providing reliability through logical preprocessing rather than complex hardware redundancy.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system implements feedback mechanisms where blade position commands are continuously validated against lead blade positions and historical data. The control computer monitors blade controller communications and adjusts commands based on validated position information, creating a feedback loop that ensures system reliability through intelligent control rather than hardware complexity.

Inventive Principle:
Principle #23Feedback

3Reliability

If blade controllers query and transmit position information amongst themselves, then loss of blade command position is reduced, but data transfer complexity increases

Engineering Contradiction:
Improveblade command position reliabilityVSAvoiddata transfer complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The control computer serves as an intermediary that coordinates position information queries and transmissions among blade controllers. Rather than creating complex peer-to-peer communication networks, the control computer centralizes the validation and distribution of blade position commands, simplifying data transfer architecture while maintaining reliability through the intermediary's coordinated management of position information.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS11008096B1Redundancy management for rotor systems with individual blade control
Publication Date: 2021.05.18 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY
  • US11008096B1 patent drawing
  • US11008096B1 patent drawing
  • US11008096B1 patent drawing

AI summary

A method and system for redundancy management of an individual blade controller rotor system is provided. The blade controller rotor system has a control computer in a stationary frame and multiple blade controllers in a rotary frame. Each of the blade controllers corresponds to a blade of a rotor system. A slip ring interfaces the stationary frame and the rotary frame. Data is transferred, via the slip ring, between each blade controller and the control computer. Each blade controller accepts and transmits information, including historical blade positions, from the other blade controllers. Each blade controller can determine a valid position for its blade based on a historical position of another blade.