Exit IDE

ZylForge Engine v4.2

CPU: 42%GPU: 88%
Engineering Intent Co-Pilot
Online
ZylForge AI CoPilot v4.2 Initialized. Integrated with ZylForge Generative CAD, Eagle Rock Telemetry, Collatz Telemetry Compression Engine, Harmonia XR, and Provenance Supply Chain Network.
Ready to design. Describe the component you need.
Constraint Engine

Active Solver: Topology Optimization

Iter: 4,092Mesh Nodes: 245000
Axial Load (F_z)
50,000 N
Shear Stress (τ_max)
420 MPa
Mass Target
≤ 0.45 kg
Material
Ti-6Al-4V
Manufacturing
5-Axis CNC
∇·σ + F = 0
σ = C : ε
ε = 1/2(∇u + (∇u)^T)
∫_Ω C_ijkl ε_kl(u) ε_ij(v) dΩ = ∫_Ω F_i v_i dΩ + ∫_Γ t_i v_i dΓ

Pipeline Status

ALL SYSTEMS NOMINAL
Intent AnalysisOK
Constraint SolvingOK
Parametric CAD GenerationOK
Volumetric MeshingOK
FEA SimulationOK
CAM Strategy generationOK
Machine G-Code OutputOK

Engineering Evidence Record

Record ID: ZF-DRONE-ARM-V1

Parametric Design

Name: AeroQuad Structural Arm (Titanium)
Material: MAT-TI6AL4V
Operations: 3 computed steps
Timestamp: 20/07/2026, 15:30:00

Simulation Validation (FEA)

Type: static_stress
Mesh Nodes: 45,210
Max Stress: 215.4 MPa
Safety Factor: 4.08x

Manufacturing Data

Method: cnc_5axis
Machine: QueenBee Pro 1515
Est. Time: 45 min
Quality Check: PASSED

Design Timeline

16:05:12
FEA Simulation passed (SF: 4.08)
16:04:45
Generated volumetric mesh (45k nodes)
16:04:10
Applied 50kN load constraint on Z-axis
16:02:33
Generated parametric topology (Ti6Al4V)
16:01:05
Received intent: 'Titanium drone arm'

Export Centre

STEP (AP242)
B-Rep for downstream CAD
STL (High Res)
Triangulated mesh for additive
Heidenhain G-Code
5-Axis toolpaths