Smart Inhaler Propellant Control for Flow Consistency

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Solution Overview

Problem

Conventional inhalers often face challenges in ensuring adequate flow through the flow channel for effective delivery of medicinal agents, particularly in cases where respiratory function is impaired, leading to inconsistent or insufficient dosing.

Innovation Solution

An inhaler system that includes a housing with a flow channel, ports for fluid communication between agent and propellant reservoirs, sensors to assess flow parameters, and a control unit to calculate and dispense additional propellant to achieve or exceed a threshold flow value, ensuring optimal delivery of medicinal agents.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional inhalers are used without flow adjustment mechanisms, then the device complexity is low, but the dosing consistency and delivery effectiveness are insufficient

Engineering Contradiction:
Improvedosing consistencyVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system employs sensors to detect flow parameters in real-time and feeds this information back to a control unit, which adjusts propellant release accordingly. This closed-loop feedback mechanism ensures consistent dosing by dynamically compensating for variations in respiratory flow, directly resolving the contradiction between dosing reliability and device complexity.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The control unit dynamically changes the parameter of propellant release amount based on detected flow conditions. By adjusting the quantity of propellant dispensed according to real-time flow assessment, the system maintains optimal dosing consistency across varying respiratory conditions without requiring overly complex mechanical structures.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If additional propellant is dispensed to compensate for insufficient flow, then the delivery effectiveness is improved, but the quantity of propellant used increases

Engineering Contradiction:
Improvedelivery effectivenessVSAvoidpropellant quantity
Core Design Contradiction:
ReliabilityVSQuantity of substance

Solution Approach 1:

The system applies partial compensation by dispensing additional propellant only to the extent necessary to achieve threshold flow values, rather than using excessive amounts. This controlled partial action ensures delivery effectiveness is improved while minimizing unnecessary propellant consumption, directly addressing the contradiction between effectiveness and propellant quantity.

Inventive Principle:
Principle #16Partial or excessive action

3Measurement precision

If real-time flow assessment is implemented, then the dosing accuracy is improved, but the measurement and control difficulty increases

Engineering Contradiction:
Improveflow measurement precisionVSAvoidflow detection difficulty
Core Design Contradiction:
Measurement precisionVSDifficulty of detecting and measuring

Solution Approach 1:

The inhaler system performs self-assessment of flow conditions through integrated sensors and automatic self-adjustment of propellant release via the control unit. This self-service capability enables precise flow measurement and dosing accuracy without requiring external monitoring or complex manual intervention, thereby reducing the practical difficulty of detection and measurement.

Inventive Principle:
Principle #25Self-service

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 system ensures consistent and effective delivery of medicinal agents by adjusting propellant release based on real-time flow assessments, improving dosing accuracy and efficacy, especially for individuals with impaired respiratory function.

Implementation Method 1

calculating an amount of propellant that will increase flow through the at least one flow channel to meet or exceed a threshold flow value

Methodology Applied
Scientific EffectPressure gradient: Pressure Gradient

Data Source

PatentUS10245393B2Methods, systems, and devices related to a supplemental inhaler
Publication Date: 2019.04.02 ELWHA LLC
  • US10245393B2 patent drawing
  • US10245393B2 patent drawing
  • US10245393B2 patent drawing

AI summary

The present disclosure relates to devices, systems, and methods that may be used to supplement inhaler use.