Magnetostatics: B, H, M, and the Self-Demagnetizing Field
Three vector fields describe a magnet, and design errors usually trace to conflating them:
B = H + 4πM [CGS: B in G, H in Oe, 4πM in G]
- M (magnetization) — dipole moment per unit volume; the material's own contribution. In a hard magnet, J = µ₀M (polarization) is what the intrinsic curve plots.
- H (field strength) — the field from external sources plus the magnet's own demagnetizing field. Inside an isolated magnet, H opposes M.
- B (flux density) — the divergence-free total. Flux lines of B are always closed loops; lines of H begin and end on the poles.
The central fact of open-circuit operation: a magnet demagnetizes itself. Its own poles create an internal field Hd opposing M:
N is exactly defined only for ellipsoids (uniform internal field), but effective values guide intuition and connect directly to the permeance coefficient: Pc = (1−N)/N.
| Shape (magnetized along…) | N | Pc = (1−N)/N | Comment |
|---|---|---|---|
| Sphere | 1/3 | 2.0 | The textbook reference case |
| Long rod, axial (L≫D) | → 0 | → ∞ | Self-protecting; operates near Br |
| Cylinder, L = D, axial | ≈ 0.36 | ≈ 1.8 | Comfortable general-purpose proportion |
| Cylinder, L = 0.25·D, axial | ≈ 0.68 | ≈ 0.47 | Thin disc — exposed; grade/temp margin critical |
| Thin plate, through-thickness | → 1 | → 0 | Worst case; survivable only in a closed circuit or with very high Hcj |
| Thin plate, in-plane | → 0 | → ∞ | Same part, rotated axis — the shape isn't the point; the axis is |
Modern NdFeB has near-linear second-quadrant behavior with recoil permeability µ_rec ≈ 1.05, so shape mostly determines the operating point, not hidden losses — until the knee. Every demag question reduces to: where does my worst-case load line cross the worst-case intrinsic curve? Chapter 4 does that calculation end-to-end.
Analytical Field Solutions You Should Have on Hand
For uniformly magnetized parts, the charge-sheet model gives closed-form fields that match FEA within a few percent for common geometries — invaluable for sanity checks and first-pass sizing. All formulas below give the axial flux density on the magnetization axis, at distance z from the pole face, for a magnet of remanence Br.
Axially magnetized cylinder (radius R, length L)
Setting z = 0 gives the pole-face center field; letting z → 0 with L ≫ R recovers B → Br/2, the theoretical ceiling for a bare pole face — a useful reality check on gaussmeter readings.
Axially magnetized ring (outer R₂, inner R₁, length L)
Rectangular block (dimensions 2a × 2b, length L, magnetized along L)
Far field: the dipole approximation
Beyond ~3 characteristic lengths, any magnet is a point dipole of moment m = M·V = (Br/µ₀)·V:
Two consequences worth internalizing: (1) at sensing distances, only m = (Br/µ₀)·V matters — a cheap large N35 beats a small N52 of lower moment; (2) doubling reach requires ~8× the moment.
Worked check — Ø10 × 5 mm N42 disc (Br = 13.0 kG): face-center field B(0) = (13000/2)·[5/√(5²+5²) − 0] = 6500 × 0.7071 ≈ 4,600 G. At z = 5 mm: 6500·[10/√125 − 5/√50] ≈ 6500·(0.894 − 0.707) ≈ 1,220 G. Field fell 73% in one magnet-thickness of travel — the 1/r³ reality of Chapter 2 in action.
Magnetic Circuit Analysis: The Reluctance Model
When soft steel routes the flux, field superposition gives way to the lumped magnetic circuit — Ohm's law with flux as current. The magnet is a flux source with internal reluctance; air gaps dominate the external reluctance; well-designed steel is nearly a short circuit.
MMF analogy: F = Hm·Lm drives Φ through ΣR
The workhorse result: gap flux density
For a magnet (length Lm, area Am) driving an air gap (length Lg, area Ag) through ideal steel, combining Ampère's law and flux conservation with the linear NdFeB characteristic gives:
Real circuits need two empirical corrections: the leakage factor k_L = Φm/Φg ≈ 1.1–3 (flux that bypasses the gap) and the reluctance/loss factor k_r ≈ 1.05–1.2 (MMF dropped in steel and joints). Compact, well-closed circuits sit near the low ends; open horseshoe-type circuits leak half their flux or more. Estimating k_L is exactly the job FEA does well (Chapter 12) — the lumped model with k_L from a quick 2D solve is a powerful hybrid workflow.
Design rules that fall out of the model
- Magnet length buys gap-driving MMF; magnet area buys flux. Match the magnet's B·H operating point to (BH)max — historically the "minimum magnet volume" condition: V_magnet ∝ Bg²·V_gap / (BH)max.
- Steel must not saturate: size cross-sections so B_steel stays under ~1.5 T (1008 steel knees near 1.6–1.8 T). A saturated yoke silently becomes an air gap.
- Series gaps add; parallel leakage steals. Every joint, plating layer, and clearance in the flux path is a series reluctance — spec joint flatness accordingly.
Demagnetization Analysis: The Calculation That Prevents Field Failures
This is the single most valuable calculation in permanent magnet engineering: verifying that the worst-case operating point stays above the intrinsic knee at the worst-case temperature. Here is the complete procedure, then a worked example.
The procedure
- Compute Pc for the magnet in its circuit (Chapter 1 factors; add the mirror-image bonus for steel backing — a magnet on a steel plate behaves like a magnet of twice its length, roughly doubling effective Pc).
- Translate properties to temperature T:
Br(T) = Br(20°C) · [1 + α·(T−20)] Hcj(T) = Hcj(20°C) · [1 + β·(T−20)]
NdFeB typical: α ≈ −0.0011/°C, β ≈ −0.0055/°C - Locate the knee at T. For sintered NdFeB, a serviceable estimate of the knee field is H_k ≈ 0.8–0.9 × Hcj(T); use the manufacturer's curve family when available.
- Compute the internal demagnetizing field at the operating point, adding any applied external field H_ext (stator reaction, adjacent magnets in repulsion, magnetizer stray fields in fixtures):
H_total = M/(Pc·µ_rec + 1) + H_ext [first term ≈ Br(T)/(µ₀(Pc+1)) for µ_rec≈1]
- Check margin: require H_total < H_k(T) with margin — 10–20% for benign products, more where a single demag event is intolerable.
Worked example: Ø10 × 2 mm N42 disc, open air, 80 °C
Br(80) = 13.0 kG·[1 − 0.0011·60] = 12.1 kG → self-field H_d ≈ Br(T)/(Pc+1) ≈ 12.1/1.22 ≈ 9.9 kOe
Hcj(80) = 12 kOe·[1 − 0.0055·60] ≈ 8.0 kOe → knee H_k ≈ 0.85·8.0 ≈ 6.8 kOe
H_d (9.9) ≫ H_k (6.8) → FAIL — permanent loss guaranteed
Fixes, checked with the same arithmetic: steel backing (mirror-image, Pc → ≈0.44) drops H_d to ≈8.4 kOe — better, but still failing against the 6.8 kOe knee; a thin open disc is that unforgiving. Stepping to N42H raises Hcj(80) to ≈11.4 kOe (knee ≈9.7) — marginal bare, but steel backing + N42H gives 8.4 vs. 9.7 kOe, a real pass with ~15% margin. Or simply thicken the magnet: Ø10 × 5 mm N42 (Pc ≈ 0.55, H_d ≈ 7.8) with steel backing (Pc ≈ 1.1, H_d ≈ 5.8) passes on geometry alone. This one page of arithmetic is why "same grade, different shape" parts fail in the field while the datasheet says they shouldn't.
Transient events count. Demagnetization is permanent even if the condition lasted milliseconds: a locked-rotor current spike, a shorted turn, ESD-scale magnetizer misfires, or two assemblies forced together in repulsion during production. Rate the magnet for the worst credible event, not the duty cycle average.
Computing Force and Torque
Magnetic force calculations come in three tiers of rigor. Use the cheapest one that answers the question.
Tier 1 — Maxwell stress on a pole face
Where flux crosses an interface at density B over area A, the tensile stress is:
For a magnet in contact with thick steel, take B as the gap/contact flux density (from Chapter 3's circuit model, including leakage) — not Br. This single formula, honestly fed, lands within ±20% of measured pull for well-behaved circuits, and it explains why the steel cup works: the cup raises contact B and adds a second working face.
Tier 2 — Virtual work / energy gradient
Differentiating gap energy vs. displacement gives force-vs-distance curves and handles shear: sliding a magnet across a plate changes overlap area, and dW/dx yields the restoring force. Shear breakaway, though, is frictional — F_slide = µ·F_normal with µ ≈ 0.2–0.3 for Ni-plate on steel — which is why rated (tensile) pull overstates sliding capacity ~4×.
Tier 3 — Magnet-to-magnet and FEA territory
Coaxial magnet pairs have exact but unwieldy series solutions; the dipole limit is the useful pocket formula:
Anything with lateral offsets, tilts, or nonlinear steel goes to FEA — but always bracket the answer with a Tier 1/2 estimate first. An FEA force that disagrees with B²A/2µ₀ by 5× is a meshing error, not a discovery.
Synchronous coupling torque
For a magnetic coupling with p pole pairs, torque follows a sine of the load angle δ (the angular lag between halves):
- More poles → stiffer coupling, lower slip angle, but faster field decay across the gap (field falls ~e^(−p·g/r)); large gaps (thick containment barriers) favor fewer poles.
- Metallic containment barriers see eddy drag ∝ speed; electrically resistive barriers (ceramic, PEEK, Hastelloy over stainless) cut that loss.
- Design slip as a feature: the coupling is a torque fuse — size T_max between worst-case process torque and the weakest downstream component.
Halbach Arrays: Theory and Practical Reality
Rotate the magnetization direction continuously along an array and the flux concentrates on one side while nearly cancelling on the other. Klaus Halbach's ideal results are strikingly clean:
Halbach cylinder (dipole, k=2): B_bore = Br · ln(r_o / r_i) — uniform field, can EXCEED Br
That second result deserves a pause: a bore field greater than the material's remanence, with no steel and no external field — r_o/r_i = e ≈ 2.72 gives B_bore = Br. Nested rotating Halbach cylinders make variable-field sources; k > 2 arrangements make quadrupoles and sextupoles for beam optics.
Engineering the real thing
- Segmentation penalty: n discrete segments per wavelength capture sin(π/n)/(π/n) of the ideal — 4 segments ≈ 90%, 8 ≈ 97%. Four per wavelength is the usual value point.
- Assembly forces are violent. Segments repel exactly where you must place them; fixtures must capture each piece positively. Assemble-then-magnetize is often impossible (the pattern needs pre-magnetized segments), so plan tooling early.
- Internal demag: some segments sit in their neighbors' reverse field — run Chapter 4's analysis per segment; corner segments often need a higher coercivity class than the rest.
- Where they earn their cost: ironless motors/actuators (no cogging, no back-iron mass), maglev and eddy-current systems, self-shielded sensor assemblies, MRI-adjacent hardware, undulators/wigglers, and torque-dense couplings.
Magnets in PM Machines: The Hard Parts
Motors and generators are the most demanding magnet application: elevated temperature, deliberate opposing fields, high-frequency flux ripple, and centrifugal load — simultaneously. Four analyses dominate magnet specification in a machine.
1 — Demag under stator reaction
The armature's d-axis field adds directly to the magnet's self-demagnetizing field. The design case is a fault: short-circuit or maximum flux-weakening current at maximum rotor temperature.
Check: H_self(Pc, T_max) + H_ext,fault < H_knee(T_max) − margin
This is why traction magnets are UH/EH class even though continuous rotor temperature might justify only SH: the spec is set by 300% current events, not steady state. Interior-PM (IPM) rotors partially shield magnets behind steel bridges; surface-PM rotors expose them fully.
2 — Eddy losses inside the magnets
Sintered NdFeB is a conductor (ρ ≈ 1.4–1.6 µΩ·m). Slot harmonics and PWM ripple induce eddy currents that heat the magnet — the nastiest kind of heat, generated where cooling is worst. For a magnet segment of width w (transverse to flux variation) below skin-effect frequencies:
Hence laminated/segmented magnets in high-speed machines: 3–6 axial (or circumferential) segments with insulating adhesive typically cut magnet loss by 70–90%. Bonded magnets, being ~100× more resistive, sidestep the problem at the cost of remanence.
3 — Skin depth sanity check
When segment size approaches δ, the simple w² scaling saturates — and so does the benefit of further segmentation. Match segmentation to the dominant loss harmonic, not to superstition.
4 — Mechanical retention
- Surface magnets need sleeves (carbon fiber, Inconel, Ti) above ~50–100 m/s tip speed; sleeve thickness trades directly against magnetic gap — a coupled electromagnetic-structural optimization.
- Adhesive selection is a temperature/lifetime spec (Chapter 9 logic); IPM bridges trade retention for leakage.
- True radial ring rotors eliminate segment-retention joints entirely for small machines — one hoop-stress calculation instead of n bond lines, and inherently balanced (Magnets 101, Ch. 7).
Grade class from fault-event demag at T_max (not average duty). N-number from torque density economics. Segmentation from the dominant flux-ripple harmonic. Coating/adhesive from rotor environment and life. Tolerances from airgap and balance budgets. Every one of these is checkable with the closed-form tools in this guide before FEA refines it.
Advanced NdFeB Materials & Processing
Coercivity engineering is where NdFeB development lives now — getting high-temperature performance with less (or no) heavy rare earth. What follows is the practical map of the modern options an advanced buyer should know by name.
Grain boundary diffusion (GBD)
Instead of alloying Dy/Tb through the bulk (which dilutes Br everywhere), GBD coats finished magnets with Dy/Tb compounds and diffuses them along grain boundaries at ~900 °C — putting the coercivity-boosting element only in the thin shell of each grain where reverse domains nucleate.
- Result: +3–8 kOe Hcj for 60–80% less heavy rare earth, with Br loss of only ~0.1–0.3 kG vs. ~0.5–1 kG for bulk alloying.
- Limitation: diffusion depth ~3–6 mm — GBD works on thin magnets (exactly the motor-segment form factor) and loses effectiveness in thick blocks.
- Spec note: GBD grades often carry manufacturer-specific suffixes; ask for the guaranteed Hcj at temperature and treat the letter grade as marketing shorthand.
The rest of the toolbox
Fine grains without milling
Melt-spun powder hot-pressed then deformed to develop texture. Grain size ~0.3 µm (vs ~5 µm sintered) yields intrinsically higher coercivity per unit Dy; net-shape ring capability (radially oriented!) makes it attractive for small high-temp rotors.
Refined chemistry, finer grains
Grain refinement, Ga/Cu/Al grain-boundary tuning, and Ce/La substitution push Dy-free material toward SH-class Hcj. Motivations are cost and supply risk (Dy/Tb export volatility); qualify against real curves, not the N-label.
Hydrogen-based recycling (HPMS)
Hydrogen decrepitation of end-of-life magnets back to alloy powder; re-sintered material now reaches within a few percent of virgin properties. Increasingly relevant for ESG-driven procurement and supply resilience.
Watch, verify, don't over-promise
SmFeN bonded (temperature-stable, high Hcj bonded alternative), additive-manufactured bonded magnets (geometry freedom, ~lower loading), thin-film and MEMS magnets. Real, useful, and narrower than the press releases suggest.
The physics scoreboard
Brown's paradox: real coercivity ≈ 20–40% of the theoretical limit — grain surfaces set the ceiling
That gap is the R&D frontier: coercivity is nucleation-limited at grain boundaries, which is why every technique above is ultimately grain-boundary engineering.
Thermal Design & Output-Drift Budgeting
Chapter 8 of Magnets 101 covered what heat does; here we quantify how to budget for it in precision systems.
Magnet material thermal properties
| Property | Value | Design consequence |
|---|---|---|
| Thermal conductivity | 7–9 W/m·K | Poor — 50× worse than copper; internal eddy heat escapes slowly |
| Specific heat | ~440 J/kg·K | Transient events heat magnets fast: 1 W in a 10 g magnet ≈ +0.23 °C/s adiabatic |
| CTE, ∥ to axis | ≈ +5×10⁻⁶/K | Strongly anisotropic — bonded joints to aluminum housings see large shear over ΔT; glue-line thickness matters |
| CTE, ⊥ to axis | ≈ −1×10⁻⁶/K (negative!) | |
| Electrical resistivity | 1.4–1.6 µΩ·m | Conductive — see eddy loss, Ch. 7 |
Flux drift budget for precision devices
Sensor and instrument designers need output stability, not just survival. Total field drift decomposes as:
- Reversible term: compensate in software (temperature sensor + α), or in hardware with Ni-Fe thermal-shunt alloys (e.g. 30% Ni "compensator" strips whose permeability falls with temperature, bypassing more flux when cold) — the classic trick in speedometers and magnetrons, still the right answer when electronics aren't available.
- Irreversible term: eliminate by thermal stabilization — bake parts 10–20 °C above worst service temperature for hours before calibration; loss taken in the factory doesn't drift in the field.
- Aging term: for properly stabilized NdFeB/SmCo, structural aging is <0.1%/decade-scale — usually below the mechanical term.
- Mechanical term: often dominant in the end: gap dimensions move with CTE; a 25 µm gap change in a 1 mm gap is 2.5% — budget the housing, not just the magnet.
SmCo's quiet superpower: temperature-compensated SmCo grades (Sm(Co,Cu,Fe,Zr) with Gd/Er substitution) achieve α ≈ ±0.001%/°C — two orders better than NdFeB — and are the default for inertial instruments, TWTs, and calibration references.
Measurement & Metrology: Trust, but Verify Correctly
Most "bad magnet" disputes are really bad measurement plans. The right instrument depends on which question you're asking.
| Method | Measures | Uncertainty | Use it for |
|---|---|---|---|
| Hysteresisgraph (BH tracer) | Full 2nd-quadrant curve: Br, Hcj, Hcb, (BH)max | ±1–2% | Material/grade qualification; the only true grade verification. Destructive-ish (needs a standard sample or cut specimen). |
| Pulsed-field magnetometer (PFM) | Full loop incl. very high Hcj | ±2–3% | High-coercivity grades beyond electromagnet saturation; faster than BH tracers. |
| Helmholtz coil + fluxmeter | Total magnetic moment m | ±0.5–1% | The workhorse of incoming inspection: fast, non-destructive, geometry-tolerant, directly proportional to what most applications use. Best per-part QC metric. |
| Gaussmeter (Hall probe) | B at one point | ±1–5% + positioning error | Relative/comparative checks, pole ID, field mapping with a fixture. Poor grade-verification tool — surface field is geometry- and probe-position-dominated. |
| Field mapper (scanning Hall / magnetic camera) | B(x,y) distribution | ~1% relative | Multipole patterns, pole transition width, dead zones, magnetization angle error — essential for encoder rings and true-radial verification. |
| Pull tester | Breakaway force | ±5–10% | Application-level acceptance; too many confounders for material QC. |
Helmholtz moment measurement — the 60-second math
Compare m against reference: m = (Br/µ₀)·V ⇒ Br_effective = µ₀·m/V
Because m is volume-integrated, it's insensitive to chips, probe placement, and minor geometry — and it catches under-magnetization and wrong-grade substitution instantly. Specify it on drawings as "magnetic moment: X mWb·mm ± 3% per Helmholtz coil" (±3% is a typical commercial magnetic tolerance; tighter costs sorting).
Statistical acceptance
- Put moment (or fixture-defined flux) under SPC like any critical dimension: X̄-R charts, Cpk ≥ 1.33 for automotive PPAP programs.
- Watch distribution shape, not just means: a bimodal moment distribution signals mixed lots or a magnetizer fixture drifting mid-run.
- Angle error (magnetization axis vs. mechanical datum, typically ±3° standard, ±1° precision) needs a rotation stage or mapper — it silently destroys sensor calibrations if unspecified.
Tolerancing & Writing a Bulletproof Magnet Specification
A complete magnet drawing controls four domains — dimensional, magnetic, material, and environmental — and states how each is verified. Here's the checklist we wish every incoming print followed.
- Standard ground tolerance ±0.05 mm; ±0.02 achievable at cost; as-sintered ±0.25 for non-critical faces.
- State whether dims apply before or after coating; give coating thickness range.
- Chamfer all edges (0.2–0.4 mm typ.) — sharp NdFeB edges chip and start coating failures.
- Flatness/parallelism only where the circuit needs it; every ground datum is money.
- Perpendicularity of pole face to axis matters for couplings/encoders — call it out explicitly.
- Material + grade + governing standard (e.g. IEC 60404-8-1) or a min-property table: Br min, Hcj min at 20 °C.
- Magnetization direction toleranced to a physical datum (±3° std); pattern drawing for multipole (pole count, transition width, index feature).
- Acceptance metric: Helmholtz moment or fixtured flux, with limits and method.
- Ship state: magnetized / unmagnetized; saturation requirement if customer magnetizes.
- Coating spec + adhesion/thickness test (cross-hatch, salt spray hours if relevant).
- Certs: material cert with actual measured properties per lot; RoHS/REACH.
- Regulated programs: PPAP level, IATF 16949 / ISO 13485 system requirements, DFARS 225.7018 melt-and-magnet sourcing where applicable.
- Max continuous + max transient temperature the part must survive in this geometry (state the assembly Pc or attach the circuit sketch — it changes the answer).
- External demag field exposure if known (motor fault spec).
- HAST/humidity or salt-spray durations for the coating system, not just "corrosion resistant."
Adding "Verify lot conformance by hysteresisgraph sample + 100% Helmholtz moment, data with shipment" to a drawing costs pennies per part and ends grade-substitution risk permanently.
Finite Element Analysis: Getting Answers You Can Trust
Modern magnetostatic FEA (Ansys Maxwell, COMSOL, Simcenter MagNet, FEMM, or the excellent open-source FEMM/Elmer for 2D) is accurate to ~1–3% — when the inputs and mesh deserve it. The failure modes are consistent and avoidable.
Model setup rules
- 2D first. Axisymmetric or planar models solve in seconds and expose 90% of design behavior. Reserve 3D for end effects, skew, and true 3D geometry (a diametral ring in a planar problem is 3D; an axial ring is axisymmetric).
- Magnet definition: linear model with Br and µ_rec (≈1.05) is correct for NdFeB above the knee. For demag studies, use the manufacturer's temperature-dependent curve family including the knee, and a solver demag model — a linear magnet can't fail, so a linear demag study is self-deception.
- Steel BH data: use measured curves for the actual alloy and anneal state; the difference between annealed 1008 and cold-worked 1008 is real flux. Never extrapolate a BH table flat — give the solver the saturated µ→µ₀ tail.
- Mesh the gap. Force and torque accuracy lives in air-gap elements: 3+ element layers across every working gap; use force via virtual work or Maxwell stress on a contour in the gap center, not on the steel surface.
- Boundary distance: outer boundary ≥ 5–10× model size, or use infinite/ballooning boundaries; a close Dirichlet boundary is an invisible steel box squeezing your field.
Validation discipline
- Reproduce a closed-form case from Chapter 2 within 2% before trusting the real model.
- Cross-check FEA force against B²A/2µ₀ using the FEA's own gap B — factor-level disagreement means mesh or contour errors.
- Mesh-refine until the answer moves <1% between refinements; report that number, not the pretty contour plot.
- Close the loop with hardware: one Helmholtz moment + one gaussmeter map on a prototype calibrates the whole model chain.
Demag post-processing shortcut: plot H·(direction of M) over the magnet volume at worst case; any region where the projection exceeds the knee field H_k(T) is permanently lost material. Element-level demag maps beat single-point checks — corners and pole edges fail first, and partial demag shows up as harmonic distortion long before gross weakness.
Advanced FAQ
How do I estimate Pc for a magnet glued to a steel plate?
Use the mirror-image method: steel of high permeability reflects the magnet, so a magnet of length L on thick steel behaves approximately like a free magnet of length 2L. Compute Pc with the doubled length (for a cylinder: Pc ≈ 1.1·(2L)/D), then de-rate slightly if the steel is thin or saturating. For two plates (magnet sandwiched), the circuit approaches closed and Pc rises steeply — usually no longer the limiting concern.
Why does my FEA force disagree with the pull tester by 30%?
The usual suspects, in order: real contact isn't ideal (surface finish, coating compliance, flatness — model a 20–50 µm effective gap and watch the numbers converge); steel BH data optimistic vs. the actual cold-worked part; pull tester alignment (off-axis pulls peel instead of tension); and gap meshing. FEA-vs-test on magnet systems should close within ~10% once an honest contact gap is included.
When is bonded NdFeB the right call in a motor despite the Br penalty?
When any of these dominate: multipole or true-radial pattern needed in one net-shape part; eddy loss in sintered segments is unmanageable at your PWM frequency (bonded resistivity is ~100× higher); assembly cost of arc segments exceeds the torque-density value; or the rotor is small enough that ring stock and insert molding beat grinding economics. Small high-speed BLDC and sensor-integrated rotors are the classic sweet spot.
Is (BH)max what I should maximize in my design?
Only when magnet volume for a given gap energy is the objective and the magnet can be biased near its (BH)max point — the classic static-circuit result. Motors often optimize elsewhere: torque scales with airgap flux and current loading, demag margin constrains the grade class, and eddy/thermal limits constrain geometry. Treat (BH)max as an energy-density index for comparing materials, not a universal objective function.
How much margin above the knee is enough?
Depends on what's uncertain. Stack the tolerances: material Hcj lot spread (−5% is common at the spec limit), temperature estimate error (±10–15 °C in rotors is honest), field calculation error (±10% lumped, ±3% good FEA), and event severity uncertainty. A 15–20% field margin at worst case covers typical commercial stacks; safety-critical or unserviceable products justify 30%+ or a coercivity class step.
Can I anneal or heat-treat NdFeB to restore a partially demagnetized magnet?
No — heat is the disease, not the cure. Restoration is magnetic: a full saturation pulse (2–3× Hcj) restores thermally or field-demagnetized material completely, provided no structural/corrosion damage occurred. Any thermal process hot enough to alter the metallurgy (>~900 °C, controlled atmosphere) is remanufacturing, not repair.
What's the practical difference between specifying flux vs. specifying Br?
Br is a material property verified on a sample by hysteresisgraph; per-part it's inaccessible non-destructively. Moment/flux is per-part measurable, geometry-inclusive, and proportional to function. Best practice: material table (Br/Hcj minima) governs the material lot; a Helmholtz moment window governs every shipped part. Specifying only Br leaves per-part magnetization unverified; specifying only flux leaves temperature capability unverified. You need both.
Do tolerances on magnetization angle really matter?
For holding, rarely. For anything that senses or synchronizes — enormously. A 3° axis tilt in a diametral encoder magnet is 3° of static angle error plus harmonic content; in a coupling it's torque ripple; in a Halbach segment it leaks flux to the "zero" side. Precision sensor programs routinely specify ±1° with mapper verification. If your device converts field direction into information, put angle on the drawing.
Engineering Support, On Call
Demag margin reviews, grade and coating selection, DFM on magnet drawings, true-radial ring feasibility, and full PPAP/ISO documentation — bring us the problem at whatever stage it's in.
Formulas provided for engineering estimation; validate designs with samples and testing.