Joint/Details
Large, singular panel adhered to 21 separate chassis tubes
16 on the bottom
3 on the catamaran section
2 on the trunk section
Other than the trunk section chassis connections, the adhered length is relatively short
The bottom is completely fixed
Materials & Form
Chassis - 4130 Chromoly Steel - hollow tubes
Panel - Carbon Fibre Composite Sandwich - ~1.5” thick molded plane
AX-5201XL carbon fibre, NOMEX honeycomb, and corresponding adhesive film for carbon fibre
Adhesive - LOCTITE EA E-120HP - pasted and compressed between the panel and chassis
Epoxy-based
Material Characteristics & Notes
4130 Chromoly Steel
Excellent strength-to-weight ratio
High tensile strength, ductility, and toughness
Lightweight in tubing form
In non-tubing form:
Modulus of Elasticity - 205 GPa
Ultimate Tensile Strength - 670 MPa
Tensile Yield Strength - 435 MPa
Rockwell B Hardness - 92
Elongation at Break - 25.5%
AX-5201XL Carbon Fiber
High stiffness, tensile strength, chemical resistance, and temperature tolerance
Low thermal expansion and weight-to-strength ratio
Excellent in tension
In general:
Modulus of Elasticity - ~230 GPa
Ultimate Tensile Strength - ~3.5 GPa
Tensile Yield Strength - ~2.1 GPa
Horrible in compression, but epoxy’s advantage in compression usually cancels that out when they form a composite
However, since we are by no means experts who manufacture our parts in a professional setting with quality equipment, I think we should lower our expectations when it comes to the material quality of not only our composites made with the Prepreg method, but the epoxy component specifically. I mean to say that the compressive counteraction that we look for in the carbon fibre composite, due to the epoxy’s presence, may not be expressed as strongly as we need it to be. Although, the NOMEX component might fix this issue.
NOMEX
High compressive strength, shear strength, materials compatibility, and fatigue strength
Low volume density and weight-to-strength ratio
High structural integrity
In general:
Ultimate Compressive Strength - ~2 MPa
Most other qualities change drastically based on stress direction
LOCTITE EA E-120HP
Superior thermal shock resistance
Excellent mechanical and electrical properties
Specifically peel and impact forces
Suitable for low stress [I wonder if that will be a problem.]
Withstands exposure to a wide variety of solvents and chemicals
Bonds dissimilar materials including aluminum, steel, and other metals, as well as a variety of plastics and ceramics
No mention of metal to organic compounds however
In general (for reinforced epoxy adhesives):
Modulus of Elasticity - ~4.5 GPa
Ultimate Tensile Strength - ~260 MPa
Tensile Yield Strength - ~230 MPa
Bonding Characteristics & Notes
Typical “Apply, Fix, and Cure” adhesive
Cavities may have been unfilled by the adhesive
Cavities created by part geometry or air bubbles created by uneven adhesive application
Clamped and cured for at least 24 hours
Known Forces or Stresses
General compressive stresses to chassis (and by extension the bottom panel) due to car parts placed on top (eg. seats)
Plus the external weight of the driver
Overloading a specific adhered tube may cause malformation and strain to the tube and adhesive, respectively
General weight of the bottom panel
We can test this if we get the approximate mass of the bottom panel
Potential Forces or Stresses
Any random stresses due to car functions (eg. the wheels being bumped into the bottom panel while turning)
Any random stresses due to the environment (eg. driving over a large rock the presses against the bottom panel)
Quality and/or Physical Concerns
Neither yet
The chassis hasn’t been adhered to the bottom panel as of right now (3:35 PM EST on Friday, July 9th), so no quality concerns
Still need to study and determine the experience of the bottom panel during car usage
Test(s)
Max stress allowed (testing the adhesive here)
Determine how much the adhesive can withstand
Tensile, compressive, and shear stress must be tested
General weight
Determine safety factor and actual strain
Needed: surface area, bottom panel mass
Testing Methods
MODS/Pre-calculations
SW
Physical
Expectations
Results
Analysis