Joint Element Shape Correction via Computer-Assisted Navigation

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Solution Overview

Problem

Current methods for correcting joint elements in surgeries, such as hip joint surgeries, lack the ability to accurately compare the desired shape with the actual shape of joint elements, making it difficult to achieve the necessary abrasion depth for preventing bone collisions and restoring the natural shape of joint elements.

Innovation Solution

A computer-assisted planning assistance method that detects and compares the actual shape of joint elements with their intended shape, using navigated and tracked pointers to plan the necessary abrasion depth, ensuring high accuracy in contour fidelity and abrasion navigation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If conventional navigation methods using pre-acquired data are used, then the surgical procedure can be performed, but the accuracy of intra-operative shape checking and abrasion depth control is insufficient

Engineering Contradiction:
Improveshape detection accuracyVSAvoidreal-time shape information
Core Design Contradiction:
Measurement precisionVSLoss of information

Solution Approach 1:

The system performs preliminary detection of the joint element's actual shape using a navigated pointer before the abrasion procedure begins. This preliminary action captures the initial geometry data, which is then stored and used for comparison throughout the surgical procedure to guide abrasion depth and monitor shape changes in real-time.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system continuously compares the detected actual shape with the intended target shape during the abrasion procedure. This feedback mechanism provides real-time information about deviations from the desired geometry, enabling the surgeon to adjust abrasion depth and maintain contour fidelity. The navigation system updates the shape comparison dynamically as abrasion progresses.

Inventive Principle:
Principle #23Feedback

2Manufacturing precision

If spherical templates are used to check femoral head sphericity, then some shape verification is possible, but systematic comparison with intended shape and monitoring of abrasion depth to necessary accuracy is not possible

Engineering Contradiction:
Improveabrasion depth controlVSAvoidshape comparison system
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent replaces conventional mechanical spherical templates with a computer-based navigation system that uses a navigated pointer to detect and digitally represent the joint element's shape. This substitution transforms manual, qualitative shape assessment into automated, quantitative measurement with precise abrasion depth control through computer-assisted planning and real-time comparison.

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

3Reliability

If no intra-operative shape detection is performed, then the surgical workflow remains simple, but the ability to navigate abrasion depth and ensure contour fidelity is lost

Engineering Contradiction:
Improvepost-operative shape accuracyVSAvoidsurgical procedure complexity
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The navigation system acts as an intermediary between the surgeon and the joint element during the abrasion procedure. The system mediates the interaction by providing real-time shape feedback and abrasion depth guidance without requiring the surgeon to directly measure or calculate geometric parameters manually. This intermediary system enhances reliability while maintaining ease of operation through intuitive navigation interfaces.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS9572630B2Planning assistance for correcting joint elements
Publication Date: 2017.02.21 SMITH & NEPHEW INC
  • US9572630B2 patent drawing
  • US9572630B2 patent drawing

AI summary

A planning assistance method for correcting joint elements is provided. In accordance with the method, the actual shape of at least one part of the joint element which is of interest is detected. The actual shape is compared with an intended shape, and the comparison data is used to plan the abrasion of joint element parts.