Lightweight Antenna Attachment Structure for Thermal Mismatch

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Solution Overview

Problem

Lightweight antenna structures face failure due to thermal and structural stresses caused by mismatched thermal expansion between the antenna and its platform, particularly in harsh environments like high-altitude balloons, where existing attachment mechanisms are inadequate in accounting for thermal mismatch and can lead to warping, misalignment, or structural failure.

Innovation Solution

An attachment mechanism using spacer elements made of stiff foam material, adhered to both the platform and the antenna panels, providing a flexible mount that insulates the panels from thermal expansion mismatch, with adhesive layers of lower yield strength than the spacer elements to absorb strain and maintain alignment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If direct adhesive bonding is used to attach antenna panels to the platform, then the attachment is simple and lightweight, but it does not account for thermal mismatch between materials causing stress and potential failure

Engineering Contradiction:
Improveantenna system weightVSAvoidjoint reliability under thermal stress
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

A foam spacer element is introduced as an intermediary component between the antenna panel and platform. This spacer absorbs differential thermal expansion through compression while maintaining the attachment, resolving the contradiction between lightweight simplicity and thermal stress reliability

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The foam spacer's compressibility parameter is utilized to accommodate thermal expansion differences. The spacer compresses under thermal load, changing its density and volume parameters to absorb stress while maintaining structural integrity

Inventive Principle:
Principle #35Parameter changes

2Strength

If rigid mechanical joints are used at the corners of panels, then structural strength is improved, but stress concentration leads to structural failure at the corners

Engineering Contradiction:
Improvestructural strengthVSAvoidcorner structural integrity
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The foam spacer acts as a flexible element that distributes mechanical loads away from corner concentrations. Its compressible nature allows it to deform under load, preventing stress concentration and improving corner integrity while maintaining overall structural strength

Inventive Principle:
Principle #30Flexible shells and thin films

3Adaptability or versatility

If lanyards or loops are used for attachment, then flexibility for thermal expansion is provided, but alignment precision is insufficient causing panels to bend or move out of place

Engineering Contradiction:
Improvethermal expansion flexibilityVSAvoidantenna panel alignment
Core Design Contradiction:
Adaptability or versatilityVSManufacturing precision

Solution Approach 1:

The foam spacer serves as a precision intermediary that provides both flexibility and alignment. Its fixed dimensions and compression characteristics ensure precise panel positioning while accommodating thermal expansion, resolving the contradiction between flexibility and alignment precision

Inventive Principle:
Principle #24Intermediary (Mediator)

4Adaptability or versatility

If the balloon platform expands or contracts due to temperature changes, then environmental adaptability is improved, but differential thermal expansion stresses the joint between balloon and antenna

Engineering Contradiction:
Improveenvironmental adaptabilityVSAvoidthermal stress at joint
Core Design Contradiction:
Adaptability or versatilityVSStress or pressure

Solution Approach 1:

The foam spacer is specifically selected to exploit thermal expansion principles. Its cellular structure allows it to compress and expand in response to temperature changes, absorbing differential thermal stress between the balloon platform and antenna panel while maintaining the joint integrity

Inventive Principle:
Principle #37Thermal expansion

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 solution effectively buffers thermal stresses, ensuring precise alignment and structural integrity of the antenna panels by accommodating differential thermal expansion, reducing the risk of failure and weight addition while maintaining precise alignment and structural support.

Implementation Method 1

A yield strength of the adhesive layers is less than a yield strength of the spacer elements

Methodology Applied
Scientific EffectElastic deformation: Elasticity

Implementation Method 2

the balloon material to expand or contract. The material of the balloon itself differs from the antenna structure and may have a different coefficient of thermal expansion

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentEP2405532B1Lightweight antenna attachment structure
Publication Date: 2014.06.11 RAYTHEON CO
  • EP2405532B1 patent drawingFigure 1
  • EP2405532B1 patent drawingFigure 2
  • EP2405532B1 patent drawingFigure 3

AI summary

The present invention relates to lightweight antenna arrays and more particularly to an attachment mechanism for attaching a lightweight antenna array to a structure. In one embodiment, an antenna structure includes a platform having a first coefficient of thermal expansion; an antenna panel having a second coefficient of thermal expansion different from the first coefficient, and having first and second opposite ends; and a support structure mounting the panel to the platform. The support structure includes a first spacer element with a first height at the first end of the panel, and a second spacer element with a second height less than the first height between the first and second ends of the panel; a first adhesive layer adhering each spacer element to the platform; and a second adhesive layer adhering each spacer element to the antenna panel. A yield strength of the adhesive layers is less than a yield strength of the spacer elements.