Panel-Insert Assembly for Sandwich Panels

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Solution Overview

Problem

Existing methods for connecting sandwich panels to airframes using mechanical fasteners with threaded inserts are hindered by long adhesive cure times, added weight, and limited pull strength, as well as the risk of gaps or unintentional pullout due to improper insert placement.

Innovation Solution

A panel-insert assembly where the insert is positioned below a skin layer with an elongated opening, allowing 360-degree contact and direct load transfer, and a method involving forming an opening in the skin layer, inserting the insert, and rotating it for alignment, facilitating a strong connection without adhesives.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If threaded inserts are potted into holes with adhesives, then the inserts are secured to the sandwich panel, but the adhesive requires long cure times, adds undesired weight, and offers limited pull strength protection

Engineering Contradiction:
Improvepull strength protectionVSAvoidadhesive cure time
Core Design Contradiction:
StrengthVSLoss of time

Solution Approach 1:

The patent removes the adhesive from the connection system entirely, extracting the problematic bonding agent that caused long cure times and weight addition. The insert is secured through mechanical means only - by being potted into a recess formed in the core material, eliminating the need for adhesive curing while maintaining structural integrity.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent replaces the chemical bonding system (adhesive) with a pure mechanical securing system. The insert is held in place through mechanical interference fit within the recess, using physical constraints rather than chemical adhesion, thereby eliminating cure time requirements and adhesive weight.

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

2Strength

If threaded inserts are potted with adhesives, then the inserts are secured to the sandwich panel, but undesired weight is added

Engineering Contradiction:
Improveconnection strengthVSAvoidpanel weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The adhesive material is completely removed from the assembly, extracting the source of unwanted weight. The connection is achieved through the recess geometry and mechanical interference fit alone, eliminating the need for additional adhesive mass while maintaining adequate connection strength.

Inventive Principle:
Principle #2Taking out (Extraction)

3Ease of manufacture

If threaded inserts are placed too high in the holes, then the inserts are easier to install, but gaps are formed reducing connection quality

Engineering Contradiction:
Improveinsert installationVSAvoidinsert placement precision
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

The recess is pre-formed in the core material at the correct depth and position before insert installation. This preliminary preparation establishes the precise final position of the insert, eliminating the need for precise placement during installation while preventing gap formation. The recess acts as a pre-positioned receptacle that guides the insert to its correct location.

Inventive Principle:
Principle #10Preliminary action

4Ease of manufacture

If threaded inserts are placed too low in the holes, then installation is easier, but unintentional pullout occurs during tightening

Engineering Contradiction:
Improveinsert installationVSAvoidinsert retention
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The recess depth is carefully predetermined during core fabrication to provide optimal insert positioning. This preliminary action ensures the insert bottom sits at the correct depth within the core, preventing both gap formation and unintentional pullout during fastener tightening, while still allowing easy insert installation.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The recess geometry parameters (depth, width, shape) are optimized to provide the correct mechanical interference fit. By adjusting these geometric parameters, the system achieves reliable insert retention without requiring precise manual placement, as the recess itself provides the positioning constraints.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS10322563B2Panel-insert assembly and method
Publication Date: 2019.06.18 THE BOEING CO
  • US10322563B2 patent drawing
  • US10322563B2 patent drawing
  • US10322563B2 patent drawing

AI summary

A panel-insert assembly including a panel having a core and a skin layer positioned over the core, wherein the skin layer defines an opening therein, and an insert positioned below the skin layer, wherein the insert is aligned with the opening.