ENGINEERING / INSPECTION PLANNING

Axial flux air-gap metrology.
Agree what passes.

Connect your functional drawing to a component inspection plan and an assembly verification scope. Decide the datums, conditions, evidence and release responsibility before approving samples.

Two rotor faces separated from a stator, with several gap measurement positions and a reminder to record temperature and load
A gap is a relationship between assembled surfaces under defined conditions. This original illustration is not a measured inspection result.

PART GEOMETRY → ASSEMBLED CLEARANCE

A cold gap measurement is one part of the evidence.

The clearance budget joins housing and bearing datums, rotor-face geometry, stator position and fastening conditions. Temperature, magnetic loading and speed can change that relationship. Keep measured component geometry, cold assembly clearance and validated operating clearance as separate conclusions.

1 / Functional datums

Identify the mounting reference, bearing axis, rotor reference face and stator locating surfaces. Document how each inspection fixture reproduces those references.

2 / Assembly condition

Specify bearings, preload, fastener sequence, shims and rotor angular position. Record where and how both gaps are measured.

3 / Operating boundary

Identify thermal growth, deflection and dynamic load assumptions. Analysis and physical test responsibility must be explicit before a safe running gap is concluded.

PROPOSED RELEASE FRAMEWORK

Four gates. A record at each decision.

These gates are a framework to agree with your project team. The quotation defines which checks, equipment, sampling and reports are included. They are not a claim that every component has completed every test.

  1. GATE / 01

    Drawing & acceptance freeze

    Agree the revision, functional datums, critical characteristics, sample plan and release authority.

    Record to agree: Controlled drawing + agreed inspection plan

  2. GATE / 02

    Material & process review

    Identify material lots, approved substitutions and the process records required for the selected component.

    Record to agree: Material documents + process/revision trace

  3. GATE / 03

    Component verification

    Measure agreed dimensions and electrical or magnetic characteristics under recorded conditions.

    Record to agree: Part-specific results + method + conditions

  4. GATE / 04

    Assembly & release review

    Where in scope, verify the assembled stack and agreed functional tests; resolve deviations before release.

    Record to agree: Assembly/test report + disposition + release

EVIDENCE MATRIX

Ask for the method beside the result.

Records to agree for component and assembly acceptance
CharacteristicRecord to agreeBoundary to preserve
Dimensions & runoutDrawing revision, datum setup, instrument identification, conditions and actual results.An instrument capability does not establish the measurement uncertainty of every part characteristic.
Stator electrical checksConnection identification, resistance temperature and agreed insulation-test settings/results.A room-temperature resistance or withstand test does not establish continuous power or insulation life.
Rotor field & balanceVector/polarity map, probe position/temperature and the agreed balance criterion/results.A field scan or balance record alone is not overspeed, containment or flight qualification.
Housing & coolingFinal-condition dimensions, sealing arrangement and agreed pressure/leak-test conditions.A component leak check is distinct from pressure-system approval and service endurance.
Assembled motorStack/preload configuration, gap locations, operating test conditions and deviation disposition.Thermal, speed, torque and life conclusions require evidence from the actual agreed test scope.

Record traceability and measurement-system suitability in the inspection plan. For calibration background, see Renishaw’s CMM calibration guidance. This reference does not establish our ownership of any particular equipment or certification.

Download the RFQ checklist

MAKE THE RELEASE CRITERIA EXPLICIT

Bring the drawing and the decision it must support.

  • Critical-characteristic list, tolerances and the document revision.
  • Datum/fixture requirements, final surface treatment and assembly condition.
  • Sample versus recurring inspection, requested records and retention needs.
  • Deviation approval, design validation and release responsibilities.

Use a non-confidential summary to begin. Request an NDA before sharing controlled drawings. A quality-plan inquiry does not constitute certification, a signed agreement or approval for an aviation, automotive or medical application.

Engineering inquiry details
Operating envelope (optional)

Enter target continuous values in the stated units. Describe peak duration, duty cycle and temperature limits in your summary. These inputs are requirements, not a product rating.

Selecting a request does not sign an NDA or confirm material availability or export clearance. We review the actual part, destination and documentation needs.

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QUALITY FAQ

Keep the conclusion within the evidence.

Does a CMM report prove the motor can run at the design gap?

No. A dimensional report covers measured geometry in stated conditions. Bearing behavior, thermal growth, rotor deflection, assembly preload and dynamic loads require a separate clearance and validation review.

Is a fixed micron-level tolerance available?

No blanket tolerance is advertised. Specify the functional characteristic, datum, geometry, material, assembly condition and measurement method. Acceptance limits and feasibility are agreed for the actual drawing.

Are all four gates included in every quotation?

No. They are a proposed planning framework. A parts-only order and an assembled motor program have different responsibilities. The accepted inspection plan identifies the included gates, records, sampling and release authority.

Can I request an NDA and material documentation first?

Yes. Start with non-confidential scope and select the relevant requests in the RFQ. NDA terms and part/destination-specific documentation are reviewed before any confidential transfer or delivery commitment.

Start from the component scope.

Published / reviewed 20 October 2026 · YokelessMotor engineering content · Proposed acceptance framework; no fabricated production results. About YokelessMotor.

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