Aerosol Article Tubular Structure for Cooling and Rigidity

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Solution Overview

Problem

Existing non-combustible aerosol provision systems face challenges in efficiently delivering aerosol while maintaining a lightweight and rigid structure, with components that can withstand high temperatures and provide optimal aerosol formation and cooling.

Innovation Solution

A non-combustible aerosol provision system comprising an article with specific tubular elements and a ratio of wall thickness to internal radius, along with overlapping paper layers and ventilation apertures, to enhance aerosol expansion and cooling, while maintaining a lightweight and rigid structure.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If the second tubular wall is made thinner to reduce weight, then the article becomes lighter, but the structural strength and rigidity are compromised

Engineering Contradiction:
Improvearticle weightVSAvoidtubular wall strength
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

The second tubular wall is constructed as a composite structure comprising an inner layer and an outer layer of different materials. The inner layer provides structural strength and rigidity, while the outer layer provides thermal insulation and chemical resistance. This composite construction allows the wall to maintain high strength despite reduced thickness, resolving the contradiction between weight reduction and strength maintenance.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

Different regions of the tubular wall are assigned different material properties according to their functional requirements. The inner portion requires high mechanical strength to maintain structural integrity, while the outer portion requires thermal and chemical resistance. By applying local quality differentiation, the design achieves optimal performance with minimal material usage.

Inventive Principle:
Principle #3Local quality

2Temperature

If the second tubular element axial length is increased to improve aerosol cooling, then aerosol cooling is enhanced, but the article length and complexity increase

Engineering Contradiction:
Improveaerosol coolingVSAvoidarticle length
Core Design Contradiction:
TemperatureVSLength of moving object

Solution Approach 1:

The second tubular element is nested within the housing structure, with its axial length extending partially within and partially outside the housing. This nesting arrangement allows the cooling function to be integrated into the existing device architecture without proportionally increasing the overall article length, effectively resolving the contradiction between cooling performance and compactness.

Inventive Principle:
Principle #7Nested doll (Nesting)

3Productivity

If the first and second tubular elements are made larger to improve aerosol formation, then aerosol formation is enhanced, but the device complexity and manufacturing difficulty increase

Engineering Contradiction:
Improveaerosol formation efficiencyVSAvoidtubular element structure
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The invention specifies precise parameter ranges for the tubular elements, including wall thickness ratios (0.05-0.5), axial length ratios (1.2-2.0), and material composition percentages. By optimizing these parameters within defined ranges, the design achieves effective aerosol formation while maintaining manufacturability and avoiding excessive complexity.

Inventive Principle:
Principle #35Parameter changes

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 achieves improved aerosol formation and cooling, with a lightweight and rigid design that facilitates easy insertion and use, while providing a temperature differential to protect temperature-sensitive components.

Implementation Method 1

aerosol-generating material section comprising aerosol-generating material and at least 5% aerosol-former material by weight of the aerosol-generating material

Methodology Applied
Scientific EffectHeating: Heating

Implementation Method 2

a first tubular element immediately downstream of the aerosol-generating material section, the first tubular element defining a first hollow cavity

Methodology Applied
Scientific EffectCooling: Cooling

Implementation Method 3

the second tubular element defining a second hollow cavity... the ratio of the volume of the second hollow cavity to the volume of the first hollow cavity can be between about 6.5 and about 8

Methodology Applied
Scientific EffectThermal energy dissipation: Heat Sink

Data Source

PatentUS20250344750A1Article for use in a non-combustible aerosol provision system
Publication Date: 2025.11.13 NICOVENTURES TRADING LTD
  • US20250344750A1 patent drawing
  • US20250344750A1 patent drawing
  • US20250344750A1 patent drawing

AI summary

An article for use in or as a non-combustible aerosol provision system includes an aerosol-generating material section including aerosol-generating material and at least 5% aerosol-former material by weight of the aerosol-generating material. The article also includes a first tubular element immediately downstream of the aerosol-generating material section, the first tubular element defining a first hollow cavity and having a first tubular wall, and a second tubular element immediately downstream of the first tubular element, the second tubular element including a second tubular wall having a wall thickness of less than about 320 μm and the second tubular element having an axial length of greater than about 15 mm.