Master Thesis · Case Study

How do you bolt a composite part to a steel bus frame — without drilling into it?

Volvo Buses was developing a lightweight composite sandwich rear cap for its city bus platform. The challenge was connecting the new composite structure to the existing metal frame without compromising the sandwich structure. My master thesis, conducted in collaboration with Volvo Buses and co-authored with Florian Ventur, developed and compared different joining concepts for this composite-metal interface.

Institution Lund University — Division of Production and Materials Engineering
Industry partner Volvo Buses (Volvo Bussar AB), Gothenburg
Type Master thesis, co-authored
Year 2022
Composite-metal joining GFRP sandwich structures FEM analysis Design for manufacture Cost modelling
CAD model of the composite rear cap joining system
CAD model of one of the joining concepts developed for the composite rear cap.
01

The problem

The existing rear cap used a conventional metal structure. The new design introduced a GFRP and PUR-foam sandwich structure, creating a fundamentally different joining problem.

Unlike conventional metal structures, sandwich composites require careful load introduction into the skins and core. The joining system therefore had to transfer loads into the composite while remaining compatible with the surrounding steel and aluminium structures.

At the same time, the solution had to remain cost-efficient, manufacturable and compatible with the production processes considered for the composite rear cap.

02

Approach

1

Characterized the existing design and defined constraints

The existing rear-cap structure was documented and used as the benchmark. Technical, manufacturing and economic constraints were then defined for the development of the new joining system.

2

Developed alternative joining concepts

Several joining principles were translated into detailed concepts for integrating the composite sandwich rear cap with the surrounding metal structure.

3

Analysed mechanical behaviour

Critical load cases and potential failure modes were investigated. Numerical analysis using ANSYS was used to compare the structural behaviour of selected concepts.

4

Built a production cost model

Material, manufacturing and assembly steps were broken down to estimate the production cost of the different joining solutions.

5

Combined the results in a decision model

Cost, weight, mechanical behaviour, supplier risk and repairability were combined in a multi-objective decision analysis to compare the concepts under different priorities.

03

The joining concepts

Insert

Metal inserts integrated into the sandwich structure and potted into the foam core, creating defined mechanical connection points for the surrounding bus structure.

Adhesive

Metal plates bonded to the composite skin using adhesive and subsequently connected to the surrounding metal frame.

Flap

Metal profiles integrated into the sandwich core before the final composite layup, creating a mechanically locked interface within the structure.

Micro-pin

A concept using small metallic pins integrated into the glass-fibre layers to create a mechanical interface between the composite laminate and the metal joining structure.

Insert joining concept
Insert concept — mechanical connection through integrated inserts.
Integrated metal flap joining concept
Flap concept — metal profile integrated into the sandwich structure.
Micro-pin joining concept
Micro-pin concept — metallic pin array integrated into the laminate.
04

How they compared

The concepts were compared across production cost, mechanical performance, repairability and supplier risk. Because the numerical analysis was not performed for every concept, the FEM results provide a comparative indication rather than a complete structural validation.

Insert Adhesive Flap Micro-pin
Estimated production cost 4,577 SEK 3,447 SEK 4,114 SEK 5,008 SEK
Mechanical performance n.a. Best Good Okay
Repairability Decent Excellent Decent Decent
Supplier risk Medium–low Low Low Medium–high
ANSYS FEM analysis of a composite-metal joining concept
Numerical analysis in ANSYS used to investigate stresses and failure behaviour in selected joining concepts.
05

Result

The adhesive concept showed the strongest overall combination of production cost and evaluated mechanical performance. It had the lowest estimated production cost and was ranked highest among the concepts included in the numerical comparison.

The flap concept remained a strong alternative. It combined comparatively good mechanical behaviour with low supplier risk and conventional metal components.

The micro-pin concept offered a more novel joining approach. However, the concept introduced higher supplier uncertainty and showed the weakest performance of the three concepts included in the numerical comparison.

The final recommendation depended on the weighting of the evaluation criteria. The multi-objective decision analysis allowed different priorities such as cost or weight to be applied instead of relying on a single fixed ranking.

Skills applied
Composite-metal joint design ANSYS FEM CAD GFRP sandwich structures Design for manufacture Cost modelling Multi-criteria decision analysis Industry collaboration