AFPM Motor DFM: Pre-Tooling Evidence Review

Build a pre-tooling evidence dossier: screen assumptions, assign manufacturing review owners and export a DFM brief. Actual yield, retention capacity and tooling cost remain unknown.

Start DFM screening ↓Reviewed 2026-11-13 · Next review target 2027-05-13

Interactive DFM Screening Engine v2026.11.13-dfm-v3

DFM Screening Evaluator

Evaluate axial attraction, disc deflection, magnet retention stresses, and tolerance stackups before cutting tooling.

Default illustrative result shown. Enable JavaScript to edit or export.View current screening result ↓One-face force proxy: 17.58 kN · Plate deflection proxy: 29.5 µm · Retention capacity: unknown.

Illustrative model only. Retention capacity is unknown; this score cannot approve production.

Design & Manufacturing Parameters

260 mm

Range: 80–650 mm

0.58

Range: 0.45–0.8

0.8 mm

Range: 0.4–3 mm

7500 RPM

Range: 200–20000 RPM

10

Range: 4–32

12

Range: 6–72

10 mm

Range: 2–30 mm

6 mm

Range: 2–16 mm

5000 units/yr

Range: 10–100000 units/yr

Heuristic Screening Score
98/ 100Lower Modeled Concern — Unverified
Tooling heuristic (not a quote): Quote Required (SMC Compaction Tooling)
Assembly Hazard: Severe (Fixture Design Required)

Maxwell Force

17.58 kN

One-face dF/dg: 6.1 kN/mm

Disc Deflection

29.5 µm

g/δ: 27.1x

Inertial Stress Scale

79.2 MPa

Capacity: not evaluated

Slot Fill Factor

54%

Fixed planning placeholder

Manufacturing Risk Analysis & Mitigation Checkpoints

warningMagnet Retention Not Evaluated

Tip speed and ρv² are demand indicators only. No selected retention method is verified by this tool.

Action: Obtain geometry-specific retention analysis, hot/aged material data and a guarded overspeed test plan before release.

warningHigh-Force Magnetic Assembly Precaution

Illustrative single-face Maxwell attraction is 17.58 kN (1793 kgf). Uncontrolled manual assembly risks severe pinch injuries and brittle sintered-magnet damage.

Action: Specify task-appropriate guarding, retained guidance and fault-safe restraint; rate the fixture using the full insertion-force envelope, not this nominal-gap proxy.

Illustrative remaining clearance: 636 µm = gap − one-disc deflection − worst-case assumed stack. Two-disc closure and dynamic loads still require validation.

Next: export this screen with drawings and request a geometry-specific review before tooling release.

Method, assumptions and score rules

Fixed assumptions: Br = 1.3 T, recoil permeability = 1.05, full annular pole coverage; effective gap = 1.15g for iron cores or illustrative 1.8g for coreless designs (actual stator thickness not supplied); steel E = 205 GPa, ν = 0.3 and uncalibrated plate coefficient k = 0.125. Tolerance magnitudes are placeholders: rotor 20(D/200), bearing 30, mounting 25(D/200), magnet 20 and thermal closure 20(D/200), all in µm. RSS combines only mechanical magnitudes then adds thermal closure linearly; no distributions or sigma level are established. Topology is RFQ context, not a topology-specific magnetic circuit or thrust solution. Pole/slot counts are recorded for RFQ only; winding compatibility and electromagnetic performance are not evaluated.

Score starts at 100. Deflection g/δ <2 / <4 / <6 subtracts 30 / 15 / 5; tolerance allowance >20% / >12% subtracts 20 / 10; bonded-only >4000 RPM subtracts 20; resin-Litz >5000/yr subtracts 15; SMC <100/yr subtracts 10. Clamp 15–98; exhausted clearance caps at 40; g/δ below 4 caps at 59. These are editorial prioritization rules, not calibrated failure probabilities. Retention capacity is excluded.

Request OEM DFM Tooling Review →

Engineering Notice: Illustrative pre-tooling screen, not production approval. Uniform one-face magnetic pressure and an uncalibrated steel plate approximation omit hub geometry, rotor coupling, temperature-dependent properties, dynamics and structural load paths. Magnet retention capacity is unknown: geometry, material allowables, bond area, interference, ageing and overspeed tests are required. No output certifies safety, cost, yield or compliance.

Engineering Boundary Caveat: Illustrative pre-tooling screen, not production approval. Uniform one-face magnetic pressure and an uncalibrated steel plate approximation omit hub geometry, rotor coupling, temperature-dependent properties, dynamics and structural load paths. Magnet retention capacity is unknown: geometry, material allowables, bond area, interference, ageing and overspeed tests are required. No output certifies safety, cost, yield or compliance.

DFM decision summary: what the screen can establish

Use the screen to prioritize review; use project evidence to release tooling.

Target Audience & Applicability Boundary

✓ Suitable For:
  • OEM engineering teams transitioning axial flux concepts to volume manufacturing
  • NPI and manufacturing directors auditing supplier DFM readiness and tooling Capex
  • Automotive EV traction, drone/eVTOL, and industrial direct-drive powertrain architects
✗ Not Suitable For:
  • DIY hobbyists performing hand-glued rewinds without precision fixturing
  • Final electromagnetic validation or safety certification
  • Universal production sign-off without material lot qualification and overspeed testing

Production release dossier: 12 evidence actions

Follow supplier trials, mechanical evidence and release ownership in commissioning order. Each action needs a named owner and a project record before tooling approval. For derivations, use the mechanical DFM theory guide.

1. AFPM producibility: turn geometry into review gates

Start with the product duty, rotor/stator architecture and load paths. Thin axial packaging trades against disc stiffness, winding access and heat removal. The table is an editorial review plan, not measured factory capability. Prioritize unresolved interfaces before specifying automation.

Suggested evidence owner
Product engineering
Record to obtain before release
Drawing revision, duty and open-action register
AFPM DFM — AFPM manufacturing review flow
Figure 1: Conceptual review flow. Swipe or focus the diagram and use arrow keys to read all steps.
InterfaceDecision evidenceNext action
AirgapDatum drawings and hot loaded clearanceAllocate a stack for each gap
Core and coilLoss, winding access and cooling trialsCompare candidate routes on the same duty
AssemblyFull force envelope and fixture fault analysisApprove guarding and retained travel
ReleasePilot measurements and signed acceptance planAssign evidence owners
Source scope and limitationsTable 1: Engineering decision matrix

2. Core fabrication routes and supplier evidence

The Somaloy 5P product guidance specifies 600–800 MPa compaction and nitrogen heat treatment up to 650°C. These are grade-specific conditions, not instructions for all SMC materials. The route comparison below is qualitative; cost, cycle time, saturation and loss must come from a selected grade and supplier trial.

Suggested evidence owner
Core supplier
Record to obtain before release
Grade-specific process trial and die review
AFPM DFM — Stator route: compare evidence, not universal rankings
Figure 2: Conceptual review flow. Swipe or focus the diagram and use arrow keys to read all steps.
RouteManufacturing trade-offRequired trial
Segmented SMC3D shapes versus die, ejection and handling constraintsGrade-specific compaction, density and core loss
Tape-wound steelDirectional flux path versus slitting and assemblyEdge insulation, stack loss and dimensional checks
PCB corelessEtched conductors versus vias and thermal limitsCurrent, resistance and temperature-rise test
Potted LitzFormed coils versus placement and encapsulation effortVoid, cure and coil-position inspection
Source scope and limitationsTable 2: Engineering decision matrix

3. Winding fill: compare like-for-like denominators

The screen assigns fixed planning placeholders: SMC 54%, tape-wound 42%, PCB 24% and resin-Litz 46%. They do not respond to slot geometry and are not manufacturing ceilings. IPC current-capacity guidance concerns conductor size and temperature rise; it does not establish those fill values. Confirm resistance, insulation damage and hot-spot temperature on pilot parts.

Suggested evidence owner
Winding supplier
Record to obtain before release
Conductor and joint trial record
AFPM DFM — Copper fill: establish comparable denominators
Figure 3: Conceptual review flow. Swipe or focus the diagram and use arrow keys to read all steps.
CandidateAccess or process riskComparable evidence
Bobbin/flyerTooth edges, bend radius and enamel damageNet copper area / declared window area
Needle/toroidalNeedle or shuttle clearanceSame denominator and insulation allowance
PCBCopper thickness, vias and dielectric volumeActive conductor area, resistance and cooling
Formed bar / LitzJoint quality, strand termination and placementJoint tests and repeatable assembly samples
Source scope and limitationsTable 3: Engineering decision matrix

4. Potting and thermal mismatch: qualify the interface

The screen has a fixed thermal allowance, not a thermal network or resin model. Material expansion, modulus, cure shrinkage and constraints jointly determine movement and stress. The following is an editorial qualification checklist; the IEC reference supports the converter-fed insulation scope, not a universal resin CTE or filler recipe.

Suggested evidence owner
Materials / insulation owner
Record to obtain before release
Encapsulation qualification record
AFPM DFM — Thermal mismatch: properties and constraints interact
Figure 4: Conceptual review flow. Swipe or focus the diagram and use arrow keys to read all steps.
InterfaceMisuse riskMitigation
Coil to housingAssuming CTE match eliminates stressUse temperature-dependent properties and constraints
Magnet to discUsing room-temperature adhesive strengthTest hot, aged bonds and representative cycles
Resin to PCBIgnoring flow, cure exotherm and voidsInspect representative potted assemblies
Source scope and limitationsTable 4: Engineering decision matrix

5. Magnet containment: demand is not capacity

Tip speed is ωR and ρv² is an inertial stress scale, not the actual bond, pocket or sleeve stress. No universal speed band makes any retention method safe. For example, the June 2016 DP760 sheet reports overlap shear of 32 MPa at 23°C and 14.8 MPa at 120°C for FPL-etched 2024T3 aluminium cured seven days at 23°C. Those coupon results are not magnet-bond allowables; substrate, cure, ageing and loads differ. Capacity remains unknown for every tool result until geometry and qualified properties are supplied.

Suggested evidence owner
Rotor structural owner
Record to obtain before release
Hot/aged retention and overspeed evidence
AFPM DFM — Retention: load path and capacity remain to be verified
Figure 5: Conceptual review flow. Swipe or focus the diagram and use arrow keys to read all steps.
ConceptUnresolved load pathVerification action
Bond onlyHot aged shear and peel, bondline variationCoupon qualification plus rotor analysis
Recessed pocketWall strength and axial captureCheck pocket geometry and contact loads
Metal ringFit, thermal expansion and axial escapeCheck interfaces, losses and containment
CFRP sleeveLayup, interference and conductive-fibre heatingCoupled structural and electromagnetic verification
Source scope and limitationsTable 5: Engineering decision matrix

6. Reproducible tolerance budget: assumptions versus capability

Report reference preset (not the initial EV preset): 240 mm OD, Di/Do 0.58, 0.9 mm gap, 9 mm steel back-iron. Load the report reference preset to reproduce this table. Values below come directly from the screening engine. Mechanical allowances are unmeasured placeholder magnitudes; RSS carries no sigma or yield claim. Thermal closure is added linearly. TIR is not a ± allowance, and two-disc movement is not solved.

Suggested evidence owner
Mechanical design owner
Record to obtain before release
Measured per-gap clearance budget
AFPM DFM — Gap closure: use a combined budget
Figure 6: Conceptual review flow. Swipe or focus the diagram and use arrow keys to read all steps.
ContributorAssumed magnitude (µm)Interpretation
Rotor axial deviation24Not measured TIR
Bearing axial allowance30Replace with assembly evidence
Stator mounting allowance30Drawing-specific datums required
Magnet thickness allowance20Bondline variation also needs assessment
Directional thermal closure24Linear addition, not random variation
Mechanical RSS + thermal76.7Illustrative combined allowance
Linear worst-case stack128Excludes one-disc deflection
Remaining clearance proxy744.3900 − one-disc deflection − worst-case stack; not validated minimum gap
Source scope and limitationsTable 6: Engineering decision matrix

7. Bearing architecture: close the full load path

Do not add the displayed one-face force directly to external thrust. Opposing disc forces may balance globally while bending each disc; actual bearing reactions depend on architecture and asymmetry. No bearing arrangement, preload shim tolerance or fatigue life is selected by this screen. Obtain supplier calculations using the full duty, fits and thermal envelope.

Suggested evidence owner
Bearing / shaft designer
Record to obtain before release
Complete duty and reaction-load review
Candidate arrangementDecision questionEvidence still needed
Angular-contact pairHow are thrust and moments reacted?Load spectrum, preload, fits and temperature
Crossed rollerDoes the compact support meet stiffness needs?Combined loads and seat geometry
Deep groove / compliant preloadAre thrust and stiffness sufficient for this duty?Rated-life and displacement calculations
Source scope and limitationsTable 7: Engineering decision matrix

8. Magnetic pull and controlled assembly

The tool uses uniform one-face pressure P = B²/(2μ₀) and force F = P·A. At assumed fields of 0.8 and 1.1 T this gives about 255 and 481 kPa; force also depends on the loaded area. Its magnetic circuit contains magnet thickness plus effective gap, so force is neither universally proportional to 1/g² nor exponential. This proxy is not an insertion-force rating or net bearing thrust.

Suggested evidence owner
Assembly tooling owner
Record to obtain before release
Guarded insertion-force and fault review
AFPM DFM — Guided insertion: retain the load under faults
Figure 8: Conceptual review flow. Swipe or focus the diagram and use arrow keys to read all steps.
UnknownWhy it mattersEvidence to obtain
Insertion path and tiltForce changes through assembly travelGeometry-specific force envelope
Pole coverage and saturationUniform annular loading is assumedCalibrated magnetic analysis
Fixture load pathNominal force omits faults and dropsRetained stops, guards and fault validation
Source scope and limitationsTable 8: Engineering decision matrix

9. Balance provisions: a transparent numerical example

For a chosen illustrative grade G = 2.5 mm/s, e = 9549G/n in µm (equivalently g·mm/kg), and U = e·m in g·mm for mass m in kg. Values below are arithmetic examples for a 4.5 kg rotor, not mandatory AFPM grades. Grade, correction planes and rigid/flexible behaviour require project selection; balance does not correct face runout or remove all vibration.

Suggested evidence owner
Balance process owner
Record to obtain before release
Correction access and acceptance record
Speed (RPM)Assumed G (mm/s)e (µm)U for 4.5 kg (g·mm)
15002.515.9171.62
60002.53.9817.90
120002.51.998.95
Source scope and limitationsTable 9: Engineering decision matrix

10. EOL access and acceptance criteria

Separate insulation qualification, routine inspection and duty validation. IEC 60034-18-41 addresses Type I converter-fed insulation; its public scope is not a universal hi-pot or surge setpoint. An approved product test plan must state voltage, waveform, duration, temperature, uncertainty and acceptance criteria. EOL coverage does not guarantee zero defects.

Suggested evidence owner
Quality / test owner
Record to obtain before release
Serial-traceable test and disposition plan
AFPM DFM — Qualification and routine EOL need different coverage
Figure 10: Conceptual review flow. Swipe or focus the diagram and use arrow keys to read all steps.
StationDFM access provisionAcceptance evidence
InsulationSafe insulated terminals and guarded contact fixtureApproved system-specific test specification
ResistanceFour-wire contact padsTemperature-corrected product limits
Back-EMFRepeatable drive coupling and sensor alignmentDeclared speed and waveform limits
Gap and runoutProbe access at specified datum/radiusLoaded hot-clearance validation plus inspection plan
Source scope and limitationsTable 10: Engineering decision matrix

11. Tooling economics: accepted units drive break-even

Mercedes-Benz reports 98 process steps in its June 2026 production announcement. That demonstrates one industrial implementation, not transferable cost savings or cycle times. For a local example only, an extra $20,000 fixed cost and $8 saving per accepted unit break even at 2,500 accepted units over the programme, not necessarily per year. Currency: illustrative USD as of this review, not a market quote. The interactive engine assigns route categories only.

Suggested evidence owner
Manufacturing / sourcing
Record to obtain before release
Dated fixed and accepted-unit cost quotes
Cost termKnown hereMinimum sourcing action
Tooling and guardingUnknown; no supplier quoteRequest scope, ownership, life and maintenance
Variable costUnknown; no measured labour or scrapQuote per accepted unit with inspection
Lifetime quantityAnnual input only; duration unknownConfirm committed demand and ramp
Route comparisonΔfixed / Δunit saving if saving > 0Include financing, rework and downtime
Source scope and limitationsTable 11: Engineering decision matrix

12. Design-freeze checklist: close unknowns before release

Use this proposed checklist to organize a project review. It is not a certification scheme or a standard-mandated set of numeric limits. A high screening score, single nominal clearance or an attractive capex estimate cannot replace approved drawings, qualification records and accountable release decisions.

Suggested evidence owner
Project release authority
Record to obtain before release
Signed evidence register before tooling
GateEvidence requiredOwner to assign
Clearance and structureSigned hot/dynamic stack and geometry-specific structural analysisMechanical engineering
Magnet containmentQualified material data, load paths and guarded validation planRotor engineering
Winding and insulationPilot process capability and applicable qualification recordsElectrical/process engineering
Assembly and EOLValidated guarded process and serialized acceptance recordsManufacturing/quality
Commercial releaseDated quotes and accepted-unit economicsProgramme sourcing
Source scope and limitationsTable 12: Engineering decision matrix

13. Illustrative Engineering Scenarios: DFM Trade-Offs & Mitigation Pathways

Four illustrative presets calculated by the same engine as the tool. These are model examples with stated assumptions, not physical case studies, measured production results or application approvals.

Illustrative preset — no physical test record

EV High-Performance Traction Motor

Baseline: 260 mm OD; Di/Do 0.58; gap 0.8 mm; 7500 RPM; back-iron 10 mm; magnets 6 mm; 5000/yr; yasa; smc_segmented_teeth; cfrp_sleeve; 10 pole pairs / 12 slots.

Core DFM Challenge:

The tight gap and series-volume target couple rotor stiffness, hot containment and repeatable coil joining. Automation needs pilot capability evidence, not a high screening score.

Recommended verification actions:

  • ▪Measure the hot loaded gap and validate both rotor supports.
  • ▪Trial the coil joining and insulation process before ordering dedicated winding tooling.
  • ▪Obtain geometry-specific retention analysis, hot/aged material data and a guarded overspeed test plan before release.

Reproducible model outputs and unknowns:

  • ✓One-face force proxy 17.58 kN; plate deflection proxy 29.5 µm.
  • ✓Remaining clearance proxy 636 µm; heuristic score 98/100 (Lower Modeled Concern — Unverified).
  • ✓Retention capacity, actual yield, cost, bearing life and certification remain unknown. Load this preset above to reproduce the arithmetic.
Illustrative preset — no physical test record

eVTOL / Drone Coreless Propulsion

Baseline: 180 mm OD; Di/Do 0.62; gap 1.2 mm; 4500 RPM; back-iron 5 mm; magnets 4.5 mm; 800/yr; torus_ns; coreless_pcb; cfrp_sleeve; 12 pole pairs / 18 slots.

Core DFM Challenge:

The coreless preset prioritizes mass, but actual PCB thickness and cooling are absent from the magnetic proxy. Neither propulsion performance nor flightworthiness is established.

Recommended verification actions:

  • ▪Replace the fixed effective-gap assumption with the real stator and rotor stack.
  • ▪Compare PCB current capacity, hot-spot temperature and rotor containment at the declared duty.
  • ▪Obtain geometry-specific retention analysis, hot/aged material data and a guarded overspeed test plan before release.

Reproducible model outputs and unknowns:

  • ✓One-face force proxy 4.65 kN; plate deflection proxy 21.6 µm.
  • ✓Remaining clearance proxy 1069.9 µm; heuristic score 98/100 (Lower Modeled Concern — Unverified).
  • ✓Retention capacity, actual yield, cost, bearing life and certification remain unknown. Load this preset above to reproduce the arithmetic.
Illustrative preset — no physical test record

Industrial Direct-Drive Pump / Generator

Baseline: 380 mm OD; Di/Do 0.6; gap 1.5 mm; 900 RPM; back-iron 16 mm; magnets 8 mm; 350/yr; torus_ns; laminated_tape_wound; recessed_pockets; 16 pole pairs / 24 slots.

Core DFM Challenge:

A larger low-speed disc still needs a full stiffness and thrust load-path assessment. External pump or generator loads and sealing requirements are outside the screen.

Recommended verification actions:

  • ▪Separate opposing magnetic forces from external thrust in a complete free-body model.
  • ▪Obtain bearing, environmental and seal qualification evidence for the actual application.
  • ▪Obtain geometry-specific retention analysis, hot/aged material data and a guarded overspeed test plan before release.

Reproducible model outputs and unknowns:

  • ✓One-face force proxy 32.45 kN; plate deflection proxy 24.2 µm.
  • ✓Remaining clearance proxy 1302.3 µm; heuristic score 98/100 (Lower Modeled Concern — Unverified).
  • ✓Retention capacity, actual yield, cost, bearing life and certification remain unknown. Load this preset above to reproduce the arithmetic.
Illustrative preset — no physical test record

High-Torque Robotic Hub Joint

Baseline: 130 mm OD; Di/Do 0.65; gap 0.7 mm; 10000 RPM; back-iron 6 mm; magnets 4 mm; 1500/yr; afir; coreless_resin_litz; recessed_pockets; 8 pole pairs / 12 slots.

Core DFM Challenge:

The AFIR resin-Litz preset combines a compact disc with high peak speed. The simplified one-face proxy does not solve the actual two-stator force balance or joint positioning accuracy.

Recommended verification actions:

  • ▪Resolve the coupled AFIR load path and hot dynamic clearance with the actual geometry.
  • ▪Validate potted coil placement, sensor alignment and the required actuator duty separately.
  • ▪Obtain geometry-specific retention analysis, hot/aged material data and a guarded overspeed test plan before release.

Reproducible model outputs and unknowns:

  • ✓One-face force proxy 2.91 kN; plate deflection proxy 3.1 µm.
  • ✓Remaining clearance proxy 604.6 µm; heuristic score 98/100 (Lower Modeled Concern — Unverified).
  • ✓Retention capacity, actual yield, cost, bearing life and certification remain unknown. Load this preset above to reproduce the arithmetic.

14. Physics Screening Engine Verification & Software Traceability

Model 2026.11.13-dfm-v3 uses deterministic arithmetic and explicit assumptions. Automated checks cover input rejection, scaling, tolerance budgets and unknown retention capacity. Software checks verify implementation behaviour; they do not validate physical accuracy. Reproduce the four examples with the named presets, inspect the method disclosure, then download the inputs, outputs and assumptions.

Return to presets and export the model record ↑
AFPM motor DFM EV preset software result showing heuristic score and unknown magnet retention capacity
Actual EV preset execution on this page, captured 2026-11-13. Software evidence only; no measured motor performance, customer outcome or production approval. Download inputs, outputs and screenshot provenance

15. Frequently Asked Questions: AFPM Motor DFM

Practical answers to 20 critical engineering, tolerancing, tooling, and commercial sourcing questions across four categories.

Build a pre-tooling review record

Which preset should start an OEM DFM review?

Choose the closest declared architecture, then replace every input with drawing and duty values. Presets are reproducible examples, not validated products or recommended application designs.

Why is the report budget different from the initial EV screen?

The report explicitly uses the 240 mm reference input set, while the initial EV preset uses 260 mm. Load the report reference preset to reproduce 128 µm worst-case and 76.7 µm mechanical RSS plus thermal allowance. Neither is measured capability.

What does a DFM brief leave unresolved?

It records geometry, duty, heuristic outputs and assumptions. Attach CAD revision, datum scheme, hot operating limits, retention evidence, inspection plan and named approval owners; the export cannot release tooling.

What happens when a required numeric field is blank?

The tool removes its prior result and disables export until all required fields are valid. A blank value is not treated as zero or a reusable previous design.

How can a reviewer reproduce a changed screening record?

Download Engineering JSON with inputs, outputs, model version and assumptions, identify the drawing revision separately, then enter the same values. The evidence screenshot records one EV preset run, not every custom design.

Commission manufacturing trials

What should an SMC supplier return before die release?

Request the selected powder grade and process sheet, compaction and heat-treatment route, die/ejection review, density and loss measurements, dimensional trial results and an itemised tooling quote. A material-family web page cannot close these actions.

Which coil trial evidence belongs in the dossier?

Use the actual conductor and enamel system. Record the conductor-area denominator, resistance, joint damage checks, thermal rise, winding access, trial quantity and rejected parts before choosing an automation route.

Does the topology selector establish a valid magnetic circuit?

No. Topology and pole/slot counts primarily record RFQ context; only limited compatibility is checked. The common one-face proxy does not solve topology-specific flux return, net bearing thrust or winding feasibility.

Does a coreless preset include the actual winding-disc thickness?

No. It substitutes an illustrative 1.8 times mechanical gap and does not accept stator thickness. Its field, force and deflection outputs cannot predict a real coreless design without a geometry-specific magnetic and structural model.

Does a winding route label prove automation is available?

No. It describes a candidate process category, not a supplier capability or quoted cycle time. Obtain trial evidence, access constraints and a scoped machine/fixture quote for the project volume.

Assign verification owners

Who closes the clearance evidence action?

The mechanical design owner combines drawing datums, measured hot/cold deviations, bearing movement and loaded structural analysis for each gap. The report reference arithmetic only shows how the assumed budget is assembled.

Can a copied score close a magnet retention action?

No. Retention capacity is not evaluated. Assign an owner for qualified hot/aged material data, radial and axial load paths, detailed geometry and the project overspeed validation plan.

What record distinguishes assembly review from running-duty review?

Use a separate assembly force-versus-travel and fault/guarding assessment. The nominal operating-gap one-face force is not a fixture rating, net bearing load or permission for manual assembly.

What must be specified before ordering a balance fixture?

Define rigid/flexible behaviour, the project-selected balance grade, service speed, correction planes, accessible correction features and the measurement method. The numerical example is not a universal G2.5 requirement.

Which EOL details need agreement with the winding supplier?

Agree test allocation, converter waveform, temperature, acceptance limits, instruments, calibration, serial traceability and failed-unit disposition. Public IEC scope alone does not supply universal hi-pot or surge limits.

Approve tooling and cost assumptions

How is accepted-unit tooling break-even calculated?

Divide additional fixed cost by the quoted saving per accepted unit across the programme horizon. The illustrative USD 20,000 divided by USD 8 equals 2,500 accepted units; it is not a market quote or annual-volume threshold.

Can low prototype volume remove an SMC die requirement?

No. A pressed SMC route still requires appropriate compaction tooling. Ask whether existing tooling, a prototype route or a new dedicated die is proposed, and quote its ownership and replacement terms.

What evidence closes a potting-process action?

Record resin grade, cure and exotherm, void inspection, insulation checks, adhesion and representative thermal/environmental cycling. Select vacuum casting, encapsulation or impregnation from those requirements; VPI is not universally mandatory.

Does the screenshot demonstrate supplier production yield?

No. It is a real software execution capture with a provenance hash, inputs and unknown retention status. Supplier yield, physical performance and customer approval require separate permissioned records.

When should the pre-tooling dossier be reviewed again?

Reopen affected actions after CAD, material, supplier, process, duty or acceptance-limit changes. This page targets a source/model review by 2027-05-13; that date is not a project qualification interval.

16. Technical References & Evidence Sources

Published · Reviewed · Next review . Published by AFPM Motor. Referenced standards and peer-reviewed literature:

  1. Gieras, Wang & Kamper — Axial Flux Permanent Magnet Brushless Machines ↗

    Springer, second edition, 2008; publisher record checked 2026-11-13

    Background on AFPM analysis, construction and applications. The public record does not validate our uncalibrated plate coefficient, heuristic score or manufacturing capability.

  2. Mercedes-Benz — Large-scale production of electric axial flux motor ↗

    Manufacturer announcement, 2026-06-09; checked 2026-11-13

    Reports production start in Berlin-Marienfelde, 98 process steps and around 30,000 m² of production space. Evidence of one industrial programme, not a site audit or proof of our cycle times, costs or yield.

  3. Höganäs — Somaloy 5P ↗

    Manufacturer product guidance; checked 2026-11-13

    For the 5P family: 600–800 MPa compaction with heated/controlled tooling and nitrogen heat treatment up to 650°C. Other grades require their own process sheet; no universal die geometry or tooling price is established.

  4. 3M — Scotch-Weld Epoxy Adhesive DP760 product data sheet ↗

    Manufacturer technical data, June 2016; checked 2026-11-13

    Temperature-dependent performance depends on substrate preparation, cure and test conditions. Temperature resistance is not a continuous-service magnet-retention allowable. Qualify the actual hot, aged bondline.

  5. ISO 21940-11:2016 — Balancing rotors with rigid behaviour ↗

    ISO, 2016; Amendment 1:2022; catalogue checked 2026-11-13

    Covers residual-unbalance tolerances, correction planes and allocation for rigid rotors. Does not cover flexible rotors or impose one AFPM balance grade based on RPM alone.

  6. IEC 60034-18-41:2014+AMD1:2019 — Type I converter-fed insulation systems ↗

    IEC consolidated edition 1.1, 2019, with 2020 corrigendum; checked 2026-11-13

    Qualification and quality-control framework for Type I PWM converter-fed winding insulation. The public scope does not establish a universal hi-pot, surge, leakage or back-EMF threshold.

  7. ASME Y14.5-2018 (R2024) — Dimensioning and Tolerancing ↗

    ASME catalogue and scope; checked 2026-11-13

    Drawing language for GD&T and datum references. Datum letters and allowable runout must be chosen for the actual assembly; this is not a source for our placeholder tolerances.

  8. IPC-2152 — Printed-board current-carrying capacity, public scope ↗

    IPC public standard excerpt; checked 2026-11-13

    Relates conductor dimensions, current and acceptable temperature rise. Does not prescribe a universal PCB-motor copper fill percentage, efficiency or production yield.

Request an OEM DFM Tooling & Producibility Review

Transitioning an axial flux motor design from simulation to repeatable series production requires disciplined mechanical tolerancing, structural disc stiffness validation, and magnetic assembly tooling. Export your DFM brief from the calculator above or send your 3D CAD step files and duty specifications to our manufacturing engineering team.

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