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ZylForge Engine v4.2
CPU: 42%GPU: 88%
Engineering Intent Co-Pilot
Online
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 NOMINALIntent 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-V1Parametric 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