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In every rotating electrical machine that uses carbon brushes — whether a DC motor, a DC generator, or a wound-rotor induction motor — brush spring thrust is the single most influential parameter governing commutation quality and brush service life. Too little pressure, and the brush loses contact with the commutator, producing destructive arcing and surface burning. Too much pressure, and both the brush and the commutator wear at an accelerated rate while operating temperature climbs. IEC TR 61015:1990 is the international technical report that standardizes exactly how this deceptively simple measurement should be performed in the laboratory.
Carbon brushes are simultaneously the most overlooked and the most critical wear components in a rotating machine. A brush operates under the delicate balance of three forces: the mechanical thrust from the spring system, the frictional drag from the rotating commutator or slip ring, and the electrodynamic forces created by current transfer across the brush-to-copper interface.
When spring thrust falls below the design value, the electrical contact between the brush and the commutator becomes unstable. At the microscopic level, the number of conducting a-spots drops sharply, forcing the remaining contact points to carry disproportionately high local current densities:
A persistent intuition among maintenance personnel is that “a little more pressure is better than a little less.” This is a dangerous misconception:
IEC TR 61015 defines the specific pressure calculation as:
where F is the measured static force (N) and A is the true cross-sectional area of the brush box (mm²). Critically, the actual contact area of the brush on the commutator or slip ring is not used in this calculation. The brush box area is a fixed design value, whereas the contact area changes continuously over the brush’s life (bedding-in, stable wear, end-of-life). Using the box area ensures consistent, comparable measurements across brush-holders and over time.
| Machine Type | Typical Specific Pressure (kPa) | Notes |
|---|---|---|
| Small DC motors (power tools) | 15 – 25 | High speed, frequent starts; favor lower end to control wear |
| Medium industrial DC motors | 18 – 28 | Most common industrial application range |
| Large mill / traction DC motors | 22 – 35 | High shock loads; favor upper end for spark prevention |
| Wound-rotor induction motors (slip rings) | 16 – 22 | Continuous duty; prioritize low friction |
| Turbo-generator excitation (collector rings) | 15 – 20 | High-speed slip rings; pressure tightly controlled |
| Crane / elevator (intermittent duty) | 18 – 28 | Static spring retention at standstill is equally critical |
IEC TR 61015 describes a carefully designed laboratory measurement procedure. Its central idea is elegantly simple: use controlled vibration to eliminate static friction (stiction) interference, approach the measurement point from two opposing directions, and average the readings to obtain a repeatable static thrust value.
The standard specifies that the test rig consists of five fundamental elements:
t and a use the nominal values of a real brush but are machined to e6 tolerance (precision fit), while dimension r is not less than the maximum r-dimension of a real brush accepted by that brush-holder.The “optimum stabilization” procedure described in Clause 5.3 is the most innovative aspect of this standard. The practical steps are:
The physics behind this procedure: when a brush slides inside its box, the direction-dependent friction introduces a bias into the measured spring force, analogous to the mechanical “backlash” phenomenon in instrument gears. By approaching the measurement point from both directions and using vibration to release the stored friction, the frictional bias is effectively averaged out, revealing the true static spring thrust.
Figure 3 of the standard elegantly illustrates this concept with a force-versus-position diagram: the upper curve (F₂) and lower curve (F₁) form a hysteresis envelope. The mean line between them, F = (F₁ + F₂) / 2, represents the true static force characteristic as a function of brush position from new to fully worn.
The note in Clause 5.5 provides a practical industrial concession: for acceptance testing of a production batch of brush-holders, the full multi-position measurement procedure is first performed on a representative sample. Once the thrust characteristic is established for that sample, the measurement for the remainder of the batch may be limited to a single brush position. This significantly improves inspection throughput in high-volume manufacturing while preserving statistical quality control effectiveness.
Freshly installed brushes must undergo a deliberate seating (bedding-in) procedure to grind the brush face to match the commutator’s curvature. Without proper seating — using a seating stone or glass-cloth abrasive strip pulled between the brush and commutator — the initial contact area may be only 10% to 20% of the nominal value. This concentrates the full current through a tiny contact zone, producing severe sparking and localized commutator overheating. After seating, the static thrust should be re-measured because the new brush height usually differs from the test brush height, changing the spring compression.
Both helical coil springs and constant-force spring mechanisms experience stress relaxation over time. In machines operating at elevated temperatures (commutator-zone temperatures can reach 120–150°C), the elastic modulus of spring materials gradually degrades. For a continuously operating industrial DC motor, spring thrust can decay by 10% to 15% within two years. This is why the IEC TR 61015 measurement methodology should also be periodically applied to in-service brush-holders as part of a condition-based maintenance program.
In multi-brush machines, thrust uniformity across all brush positions is critical. Industry practice typically calls for ±10% maximum deviation within the same polarity group. Non-uniform thrust distribution causes some brushes to carry a disproportionate share of the total current (lower contact resistance from higher thrust attracts more current), accelerating those brushes’ wear and creating a “weakest link” failure pattern.
Q1: How does IEC TR 61015 relate to IEC 60136 (brush dimensions)?
IEC 60136 specifies the physical dimensions and tolerances of carbon brushes, while IEC TR 61015 specifies how to measure the thrust applied to those brushes by the brush-holder pressure system. They are complementary: IEC 60136 defines the geometric envelope of the brush, and IEC TR 61015 ensures that, within that envelope, the spring system delivers the correct mechanical thrust. Additionally, IEC 60560:1977 provides the terminology for brush-holders and is directly referenced within IEC TR 61015.
Q2: Why does the standard mandate a measuring device displacement of no more than 0.2 mm?
A helical spring’s force-displacement relationship follows Hooke’s Law (F = k × Δx). If the measuring device itself deflects significantly under load — say, 2 mm — it is effectively adding an extra compression (or relaxation) to the spring during the measurement, shifting the reading away from the true thrust at the spring’s actual working height. Limiting device displacement to 0.2 mm keeps this systematic error below approximately 1%.
Q3: Do constant-force spring mechanisms still need to be tested per this standard?
Absolutely. Although constant-force springs are designed to deliver near-uniform thrust across the full stroke range, manufacturing tolerances, material batch variations, and long-term stress relaxation all cause actual force values to deviate from nominal. The IEC TR 61015 method applies to all types of brush-holder pressure systems — helical coil, constant-force (clock-type), torsion spring, or otherwise — regardless of their design principle.
Q4: How can I approximate brush thrust adequacy in the field without a full test rig?
In field conditions where a standard-compliant test rig is unavailable, a practical approximation can be achieved by: using a calibrated electronic force gauge (±1% accuracy), aligning its probe with the thrust axis at the brush top center, slowly pulling the brush until it just begins to move, while gently tapping the brush-holder body to simulate the standard’s vibration effect. Take readings at three positions (new, mid-wear, wear limit). This method does not replace a proper laboratory measurement, but serves effectively for trend monitoring and anomaly detection.