Exoskeleton Actuator Structure for Misaligned Load Back Drive

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Solution Overview

Problem

Existing linear actuators face issues with back drive and lack of flexibility due to misaligned loads, particularly when converting rotary motion to linear motion, as they do not allow for bi-directionality and efficient force application off-axis from the screw axis, limiting their use in compact applications.

Innovation Solution

A linear actuation device with a threaded shaft and a movable element constrained by guiding rods and ball joints, allowing rotation to translate linearly while preventing transverse moments and enabling force application misaligned with the shaft, ensuring continuous operation and bi-directionality.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If a screw-nut assembly is used for converting rotary motion to linear motion, then the actuator can achieve compact dimensions, but it cannot handle misaligned loads without back drive problems

Engineering Contradiction:
Improveactuator dimensionsVSAvoidback drive performance
Core Design Contradiction:
Volume of moving objectVSReliability

Solution Approach 1:

The patent introduces a movable element with a cavity that receives the threaded shaft, acting as an intermediary between the screw mechanism and the load. This movable element can translate along the shaft axis while accommodating misaligned forces, preventing direct transmission of transverse moments to the screw-nut assembly and eliminating back drive issues while maintaining compact dimensions

Inventive Principle:
Principle #24Intermediary (Mediator)

2Device complexity

If the nut screw is rigidly connected to the load component, then the structure is simplified, but misaligned loads cause binding and loss of reversibility

Engineering Contradiction:
Improvestructural complexityVSAvoidflexibility of use
Core Design Contradiction:
Device complexityVSAdaptability or versatility

Solution Approach 1:

The patent employs two guiding rods that are movable relative to the movable element, constrained only in the axial direction. This dynamic arrangement allows the guiding rods to automatically adjust and accommodate misaligned loads, enabling the actuator to handle off-axis forces without binding while maintaining simple structure and full reversibility

Inventive Principle:
Principle #15Dynamics

3Reliability

If linear rails are added to constrain the nut screw, then misalignment problems are reduced, but the actuator still cannot eliminate back drive issues and complexity increases

Engineering Contradiction:
Improvealignment stabilityVSAvoidactuator structure
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent divides the movable element into first and second elements constrained with each other, where the first element couples to the threaded shaft and the second element couples to the guiding rods. This segmentation allows independent optimization of each component's function, achieving reliable alignment stability through the guiding rods while keeping the overall structure simpler than traditional linear rail solutions

Inventive Principle:
Principle #1Segmentation

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

The solution enhances back drive operation and flexibility, allowing for compact and reversible actuation with continuous translation and reduced binding, enabling applications with misaligned force application and minimizing overall dimensions.

Implementation Method 1

a threaded shaft (2) connected at one end to driving means intended to allow the threaded shaft to rotate about its longitudinal axis, and a movable element (3) provided with a cylindrical cavity, intended to receive the threaded shaft, and configured such that a rotation of the threaded shaft corresponds to a translation of the movable element along the longitudinal axis

Methodology Applied
Scientific EffectScrew mechanism: Screw

Implementation Method 2

two guiding rods (4, 4') coupled to the movable element and constraining the translation thereof along a direction parallel to the longitudinal axis

Methodology Applied
Scientific EffectMechanical constraint:

Implementation Method 3

the portion and the seat are shaped such that the contact between the seat and the portion occurs in a contact area within a plane comprising the longitudinal axis and it is parallel to the plane comprising the development axes of the two guiding rods

Methodology Applied
Scientific EffectGeometric constraint: Geometry

Data Source

PatentEP3443242B1Actuator for exoskeleton
Publication Date: 2021.10.06 FOND INST ITAL DI TECH
  • EP3443242B1 patent drawingFigure 1~2
  • EP3443242B1 patent drawingFigure 3~4c
  • EP3443242B1 patent drawingFigure 5~6

AI summary

The present invention relates to an actuation device (1) comprising a threaded shaft (2) connected at one end to driving means adapted to allow the threaded shaft (2) to rotate about its longitudinal axis (a). The device further comprises a movable element (3) provided with a cylindrical cavity (30) adapted to receive the threaded shaft (2), and configured in such a way that a rotation of the threaded shaft (2) corresponds to a translation the movable element (3) along the longitudinal axis (a). The device (1) further comprises two guiding rods (4, 4') coupled to the movable element (3) and adapted to constrain the translation of the latter along a direction parallel to the longitudinal axis (a). The movable element (3) comprises a first (31) and a second (32) element constrained to each other, wherein the first element (31) is coupled to the threaded shaft (2) and the second element (32) is coupled to the two guiding rods (4, 4'). A portion (320) protrudes from the second element (32) adapted to fit into a seat (312) formed in the first element (31), and wherein the portion (320) and the seat (312) are shaped in such a way that the contact between the seat (312) and the portion (320) takes place in a contact zone that extends along a section of the portion (320) whose midpoint lies in a plane that comprises the longitudinal axis (a) and is parallel to the plane which comprises the development axes (β,β ') of the two guiding rods (4, 4').