Multifaceted Rotary Tool Thermoforming for Aircraft Panels

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current methods for manufacturing aircraft sidewall and ceiling panels using thermoset composite materials are inefficient due to long fabrication cycles, material waste, high disposal costs, and inability to integrate uniform decorative textures, while lacking the capability for single-stage processing and net size part fabrication, resulting in part-to-part variability and residual stresses.

Innovation Solution

A thermoforming system utilizing a forming press with multifaceted mold tooling, where a thermoplastic material is preheated and formed into a pressed part using a rotary tool with multiple faces, allowing for continuous processing and finishing operations, enabling the integration of additional materials and decorative textures, and facilitating rapid tool changes and scrap recycling.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Quantity of substance

If conventional thermoset composite methods are used, then parts can be fabricated with complex materials, but fabrication cycle time becomes excessively long and productivity is low

Engineering Contradiction:
Improvematerial complexityVSAvoidfabrication cycle time
Core Design Contradiction:
Quantity of substanceVSProductivity

Solution Approach 1:

The patent changes the fundamental material parameter from thermoset to thermoplastic composite materials, enabling single-stage processing and dramatically reducing fabrication cycle time while maintaining the ability to handle complex material configurations

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent segments the multi-stage thermoset process into a single integrated thermoplastic forming stage, eliminating intermediate processing steps and reducing overall fabrication time

Inventive Principle:
Principle #1Segmentation

2Shape

If conventional thermoset methods with multiple processing stages are used, then complex composite configurations can be achieved, but material waste and disposal costs increase

Engineering Contradiction:
Improvecomposite configuration complexityVSAvoidmaterial waste
Core Design Contradiction:
ShapeVSLoss of substance

Solution Approach 1:

Changing from thermoset to thermoplastic materials allows for net-size forming without excessive trimming, as thermoplastics can be formed directly to final dimensions and trimmed waste can be recycled

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent enables recovery and recycling of trimmed thermoplastic material, converting what would be waste into reusable feedstock, thereby reducing material loss

Inventive Principle:
Principle #34Discarding and recovering

3Quantity of substance

If conventional tooling methods are used, then parts can be manufactured, but tool change-over time becomes lengthy and adaptability is reduced

Engineering Contradiction:
Improvepart productionVSAvoidtool change-over time
Core Design Contradiction:
Quantity of substanceVSAdaptability or versatility

Solution Approach 1:

The patent employs dynamically interchangeable mold inserts that can be quickly swapped during production, allowing rapid adaptation to different part configurations without lengthy tool change-overs

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The press tooling is designed with universal interfaces that accommodate multiple mold insert configurations, enabling a single tooling system to produce various part types

Inventive Principle:
Principle #6Universality (Multi-functionality)

4Quantity of substance

If conventional uniform temperature field processing is used, then existing composite configurations can be processed, but new materials with highly variable thermal properties cannot be effectively fabricated

Engineering Contradiction:
Improvematerial compatibilityVSAvoidthermal processing control
Core Design Contradiction:
Quantity of substanceVSManufacturing precision

Solution Approach 1:

The patent implements localized heating zones with independently controllable temperature fields, allowing different regions of the workpiece to receive appropriate thermal treatment according to their specific material properties and geometric requirements

Inventive Principle:
Principle #3Local quality

5Quantity of substance

If conventional fabrication methods are used, then parts can be produced, but part-to-part variability increases and requires repairs

Engineering Contradiction:
Improvepart productionVSAvoidpart-to-part variability
Core Design Contradiction:
Quantity of substanceVSManufacturing precision

Solution Approach 1:

The patent incorporates feedback control systems that monitor processing parameters in real-time and automatically adjust conditions to maintain consistent part quality and minimize variability

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent replaces manual assembly operations with automated robotic systems, eliminating human variability and improving part-to-part consistency

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 approach reduces material waste, eliminates the need for extensive tooling and preheating, and allows for efficient production of parts with integrated textures and reduced part-to-part variability, improving manufacturing efficiency and flexibility.

Implementation Method 1

feeding a thermoplastic material into a preheating oven to form a preheated thermoplastic material

Methodology Applied
Scientific EffectThermal heating: Heating

Implementation Method 2

feeding the preheated thermoplastic material into a forming press to form a pressed thermoplastic part

Methodology Applied
Scientific EffectMechanical compression: Compression

Data Source

PatentUS11235508B2Modular thermoforming system
Publication Date: 2022.02.01 THE BOEING CO
  • US11235508B2 patent drawing
  • US11235508B2 patent drawing
  • US11235508B2 patent drawing

AI summary

A thermoforming system and related methods for manufacturing thermoplastic parts, such as interior panels for aircraft, may include a roll-to-roll operation and a forming press having at least one selectively rotatable tool. The rotatable tool, which may include a mold and/or a die, may be multifaceted, such that different faces of the tool have different mold arrangements for different forming characteristics.