Aircraft Actuator System Using Hydromechanical Spool Feedback

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Solution Overview

Problem

Aircraft actuator systems face challenges in achieving predictable movement of control-surface components across varying operating conditions without incurring excessive weight and size penalties.

Innovation Solution

The actuator system employs a valve assembly with concentric spools, where the inner spool is directly driven by a motor converting current into mechanical movement, and the outer spool is hydromechanically moved, utilizing sensed position data to regulate current for precise control, thereby avoiding direct amplification and minimizing weight and size.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional actuator systems use larger components or additional mechanisms to achieve predictable movement across varying operating conditions, then reliability and performance consistency improve, but weight and size increase

Engineering Contradiction:
Improvepredictable movement consistencyVSAvoidactuator system weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent employs feedback through position sensors that detect the actual position of control surfaces and feed this information back to the flight control computer. The computer compares sensed position data with commanded position data and adjusts motor current accordingly, enabling consistent and predictable actuator performance across varying operating conditions without requiring excessive weight or size in the actuator components themselves.

Inventive Principle:
Principle #23Feedback

2Reliability

If conventional actuator systems use larger components or additional mechanisms to achieve predictable movement across varying operating conditions, then reliability and performance consistency improve, but device size increases

Engineering Contradiction:
Improvepredictable movement consistencyVSAvoidactuator system size
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent employs feedback through position sensors that detect the actual position of control surfaces and feed this information back to the flight control computer. The computer compares sensed position data with commanded position data and adjusts motor current accordingly, enabling consistent and predictable actuator performance across varying operating conditions without requiring excessive weight or size in the actuator components themselves.

Inventive Principle:
Principle #23Feedback

3Measurement precision

If direct drive assembly is controlled by sensed position data to regulate current, then control precision improves, but device complexity increases

Engineering Contradiction:
Improvecontrol precisionVSAvoidcontrol system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The control system receives feedback from position sensors and uses this information to regulate motor current through the flight control computer. The computer compares sensed position data with commanded position data and adjusts current accordingly, achieving precise control while keeping the actuator hardware itself relatively simple.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The flight control computer serves as an intermediary between the position sensors and the motor drive assembly. It processes the feedback information and generates appropriate control signals, decoupling the sensing and actuation functions while enabling precise control through software-based regulation rather than complex hardware circuits.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 solution enables consistent and dependable performance of the actuator system across diverse operating conditions, ensuring accurate control-surface movement without the need for excessive weight or size, by using a direct drive assembly controlled by sensed position data for precise fluid flow management.

Implementation Method 1

an inner spool being directly driven by a motor that converts current input into mechanical movement

Methodology Applied
Scientific EffectElectromagnetic conversion: Electromagnetic Induction

Implementation Method 2

The outer (larger) spool is not directly driven, but instead is hydromechanically caused to move upon movement of the inner spool

Methodology Applied
Scientific EffectHydraulic pressure differential: Hydraulic Press

Data Source

PatentUS8474486B2Actuator system
Publication Date: 2013.07.02 PARKER INTANGIBLES LLC
  • US8474486B2 patent drawing
  • US8474486B2 patent drawing
  • US8474486B2 patent drawing

AI summary

An actuator system (14) comprising a valve assembly (40) having an inner spool (50), an outer spool (60), and a sleeve (70). An assembly (80) directly drives the inner spool (50) to move it relative to the outer spool (60), and thereby hydromechanically causes the outer spool (60) to move relative to the sleeve (70). A control assembly (90) provides current input to the drive assembly (80), which converts current input into mechanical motion. The control assembly (90) senses the position of the inner spool (50) and regulates current in accordance with the sensed position.