The problem
Composite designs don’t translate — print them naively and the part gains weight.
The internal load path has to be redesigned into additive-optimal ribbing first. That’s the slow, specialist-dependent step. It’s the problem we solve.
The process
Send us a part. Get back additive-optimal ribs.
01
Send us your part
Solid, shell, or your carbon-fiber / foam design. The outer mold line stays fixed.
02
We generate the ribs
Additive-optimal internal structure, output as clean B-rep STEP — in minutes.
03
It drops into your CAD
Split, join, and edit downstream — then print in-house or at a bureau.
The solution
Three things you keep when the ribs come back.
Your OML
untouched
Your aero surface never moves. Your existing carbon-fiber or foam part is the starting point — we re-engineer only the inside.
Minutes
not days
Per part — compounding across the 15 to 30 structural parts of an airframe. Alternatives take hours to days.
Clean CAD
not mesh
Real B-rep solids in STEP. Split and join drop into SolidWorks or Fusion intact.
Where we sit
Rib generation, compared.
Manual CAD
Rhino + GH
nTop
InfinitForm
Time to proficiency
Have it
6–12 months
2–4 months
Days
Time per part
Hours–days
Hours–days
Hours–days
Minutes
Output
Unoptimized
Polysurface soup
Mesh / lossy
Clean B-rep STEP
Downstream edit
n/a
Fights you
Messy
Split & join work
Close ✕
Close ✕
// Request a rib generation
