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Design Guide · Lightweighting

Reduce mass.
Topology + material.
Weight optimization.

Design for lightweighting reference. Topology optimization, material substitution, lattice structures. Aerospace, racing, EV applications.

01 · Key principles

Key principles.

Topology optimization

FEA-driven

FEA optimizes mass distribution. Generative design.

Material substitution

Composite for metal

Carbon fiber composite for steel. Aluminum for steel.

Lattice structures

Internal porosity

3D printed lattices replace solid sections.

Hollow design

Internal cavities

Hollow components vs solid where possible.

Cross-section

I-beam vs solid

I-beam efficient stiffness/mass. Tube hollow.

Composite materials

Carbon fiber

Composite for highest stiffness-to-mass.

FAQ

Topology optimization?

FEA finds optimal mass distribution for given loads. Generative design tools.

Carbon fiber vs aluminum?

Carbon fiber 1.5 g/cm³ vs aluminum 2.7 g/cm³. ~50% lighter at equivalent stiffness.

Lattice 3D printing?

Internal lattice structures replace solid. 30-70% mass reduction. Aerospace standard.

Cost vs weight savings?

Lightweighting typically 30-100% cost premium. Per industry priority.

Manufacturing constraints?

3D printing enables lattice. Composite layup specialty. Per process.

Validation?

FEA + physical testing. Mass-stiffness-strength all verified.

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