Carbon Fibre Internal Structures
Owned end-to-end geometric integration, load-path optimisation, analysis, and manufacture of Solar Car 4’s primary chassis structure
Overview
Solar Car 4’s internal structure is a set of unidirectional capped carbon sandwich “I-beam” bulkheads. They form the primary load-bearing structure onto which most systems are mounted, interfaced, and loads reacted. I was responsible for this subsystem from collating system requirements to geometric interfacing and load analysis, to a manufactured race-ready assembly. The result was a stiff and robust structure that survived the real-world validation of driving down the Stuart Highway, enabled easy servicing, while weighing around 18kg total – less than 10% of the car’s weight.
Photo of exposed car internals at the Motor Vehicle Inspection Facility in Darwin
The systems problem
The design of the internal structures is fundamentally a systems integration problem, as they react and interface the loads/geometry of almost all the subsystems on the car.
The bulkheads are the direct mounting point for six high-load subsystems:
The bulkheads also provide the geometric interface for many more mechanical and electrical systems:
As a systems engineering problem, I needed to liaise across subteams, across many people and subsystems that had arrived at their own conclusions on ideal geometry, constraints and loads. I needed to reconcile systems and resolve conflicts all while attempting to achieve my own objectives in reducing weight and cutting down the number of bulkheads (everyone has an ideal bulkhead position, but we don’t want there to be 50 of them in the car! There are trade-offs that needed to be justified and made). After geometric and functional requirements, I re-calculated and re-ran all load cases to cross check and produce a consistent methodology for analysis, before moving into detailed composites design.
Structural bulkheads highlighted in purple
Geometric design
The capped “I beam” design is unusual in the world of solar cars, but was a deliberate choice made as a trade-off between serviceability and optimisation. Solar Car 4 was our team’s first asymmetric catamaran, and also the first time we were designing every structural and mechanical system in-house. This drove a clear priority: modular design that enables fast geometric change, as well as easy serviceability in its usage condition. As such, a beam structure was the natural architecture of the system, compared to semi-monocoque “torsion box” systems that are often seen in other teams (better weight optimisation, worse modularity, worse serviceability).
In future, a “torsion box” may be the better option to optimise load paths and trim weight, but given the inexperienced team I was working with, with constant revisions to subsystem requirements, and a team that was learning composites for the first time, I believe I made the right choice to use beams. It let us keep iterating up until very late into the timeline, without large re-tooling constraints that would otherwise hinder our development.
Early geometric option exploration (left). Final bulkheads with subsystems integrated (right)
Analysis under uncertainty
The bulkheads are slender longitudinally, with suspension limited to a small vertical mounting distance high-up, which makes the suspension assembly act as a large moment arm (~500mm vertical from contact patch to lower A-arm, while the A arms are only mounted ~150mm apart). This saw immense reaction forces on individual arm mounts – 5kN+ with a large out-of-plane component.
FBD of representative front suspension reaction forces
We had no measured suspension load data, and outback highway conditions are unpredictable and often catch out even the best of teams anyway – delaminating mounting structures or snapping suspension arms. Furthermore, as an inexperienced team with constantly changing parameters, I decided not to run an inertial-relief simulation typical of this use-case, as I cannot validate or even be confident of the unknowns of final mass and placement. With the many uncertainties in design, and the practical inability to validate them until the car is driving (at which point it is too late to change anything), I chose to design against conservative representative worst case static cases. Fixed displacement constraints on the occupant cell capture loads going through the transverse bulkheads, while triangulated displacement constraints across the contact patches capture loads through the diagonal bulkheads. The whole structure was designed to the materials factors of the EuroComp composites design code, which by recommendation in consultation with professional engineers, sets a standard for a safe and robust first in-house composites structure.
Composites design followed a quick to detailed workflow:
Some first-pass sizing was conducted using the Rule of Mixtures approach in an Excel spreadsheet to provide some initial design outputs, getting an idea of the stresses and deflections at play for the loads experienced.
Excel RoM analysis
Detailed FEA was conducted using Ansys Mechanical with ACP composites layup modelling. Suspension loads were modelled through a representative beam element model. A shell model was used to model the bulkheads, including the unidirectional capping to form the I beam, shear patches, and foam and solid core replacements. A range of load cases were analysed, including various suspension and internal mounting loads.
Suspension beam element representation (left). Bump load composite failure analysis on FE model (right)
Hand calculations were used to work around the limitations of the shell element mesh, validating the strength of bonding and overlaminate joints between bulkheads, validating shear patch and core insert capabilities, and justifying points of artificially high stress.
Manufacturing
Manufacturing the bulkheads was a job split between our in-house workshop and our composites manufacturing partner Sydney Composites. I led, and was responsible for, the manufacturing of the transverse and diagonal bulkheads (the ones that take most of the suspension and subsystem loads) out of prepreg carbon fibre. Sydney Composites resin-infused the 4m long longitudinals and the side bulkheads.
Our in-house prepreg bulkheads under a vacuum debulk on a flanged glass table
Snippet of bulkhead cross section from engineering drawing
Researching manufacturing options early in the design process, I committed to a tooled-flange process. This involved building flanges onto a glass table, laying up an outer face sheet that covers the height and curves around the top, laying in unidirectional capping and the core, as well as any core inserts, placing in a foam (note change from drawing) former to round the corner, then closing off with an inner face sheet that ties all previous plies together. Final fitment was done with Sydney Composites. Bulkheads were bonded together with Spabond-445 structural epoxy, with epoxy fillets throughout. High load areas had epoxy bonding reinforced with 400gsm biaxial overlaminates.
Bulkhead fitment at Sydney Composites
Results
The completed bulkhead assembly weighs around 18kg before bonding into the aeroshell, which is within comparable range to equivalent structures on the best international teams. Despite the 50% car size increase, it still helped to trim weight overall, and it ran reliably without needing repairs across ~2000km of outback roads (1301km in race conditions), over unpredictable cattle grids, the occasional off-road excursion, and many times around the Hidden Valley Racetrack in Darwin.
Final assembled bulkheads pre subsystem integration
The car's internals catching some fresh air in Coober Pedy
Cattle grids are no problemo!