Servovalve Mechanical Feedback for Sensorless Position Control

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Solution Overview

Problem

Conventional servovalves with linear actuators face reliability issues due to the use of expensive power electronics for position feedback, which also increase size, weight, and vulnerability.

Innovation Solution

A servovalve design incorporating a pilot stage with a hydraulic ejector and receiver, utilizing a piezoelectric linear actuator and a mechanical feedback system via a lever with a force transfer interface, eliminating the need for movement sensors by providing entirely mechanical feedback.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If power electronics and movement sensors are used for position feedback in servovalves with linear actuators, then position control capability is improved, but reliability deteriorates and cost increases

Engineering Contradiction:
Improveposition control capabilityVSAvoidsystem reliability
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The patent replaces electronic position feedback systems with a mechanical feedback rod that directly couples the power-directing member to the pilot stage. This mechanical coupling provides position feedback through pure mechanical means, eliminating movement sensors and power electronics while maintaining position control capability. The feedback rod transmits positional information mechanically from the power stage back to the pilot stage, resolving the contradiction between measurement precision and reliability.

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

2Measurement precision

If power electronics and movement sensors are used for position feedback, then position control capability is improved, but device complexity and weight increase

Engineering Contradiction:
Improveposition control capabilityVSAvoidelectronic component complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent substitutes complex electronic position feedback components with a simple mechanical feedback rod. This rod provides direct mechanical coupling between the power-directing member and the pilot stage, transmitting position information without requiring sensors, signal processing electronics, or complex control circuits. The mechanical system achieves position control capability while dramatically reducing device complexity.

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

3Measurement precision

If power electronics are used for feedback control, then position control capability is improved, but cost increases

Engineering Contradiction:
Improveposition control capabilityVSAvoidmanufacturing cost
Core Design Contradiction:
Measurement precisionVSEase of manufacture

Solution Approach 1:

The patent replaces expensive power electronics and movement sensors with an inexpensive mechanical feedback rod. This rod can be manufactured from simple materials and requires no electronic components, signal processing circuits, or sophisticated control systems. The mechanical feedback system achieves position control capability at a fraction of the cost of electronic systems.

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

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 design enhances the reliability of the servovalve by using mechanical feedback, improving vibration behavior and reducing the reliance on costly electronic components, thus enhancing overall performance and durability.

Implementation Method 1

utilizing a piezoelectric linear actuator

Methodology Applied
Scientific EffectPiezoelectric effect: Piezoelectric Effect

Implementation Method 2

a hydraulic element for ejecting a jet of fluid and a hydraulic element for receiving the jet of fluid

Methodology Applied
Scientific EffectHydraulic jet: Jet

Data Source

PatentUS11994154B2Servovalve having a linear actuator and mechanical feedback
Publication Date: 2024.05.28 SAFRAN AEROSYST
  • US11994154B2 patent drawing
  • US11994154B2 patent drawing
  • US11994154B2 patent drawing

AI summary

A servovalve having a pilot stage includes two hydraulic elements that are movable relative to each other so as to move a power-directing member, the pilot stage including a linear actuator having a main pusher arranged to modify the relative position of the hydraulic elements. The pilot stage has a position feedback lever.