Planetary vs. Cycloidal Gearboxes for AGV and AMR Drive Wheels: Shock Load Withstand, Radial Overhung Load, Backlash Drift, and Sizing Trade-Offs
Published: 2026/11/03Last reviewed: 2026/11/03

Planetary vs. Cycloidal Gearboxes for AGV and AMR Drive Wheels: Shock Load Withstand, Radial Overhung Load, Backlash Drift, and Sizing Trade-Offs

Compare planetary vs cycloidal AGV drive wheel gearboxes for shock torque, radial loads and backlash. Use the sizing example and RFQ checklist to shortlist.

For planetary vs cycloidal AGV drive wheel gearboxes, shortlist by wheel torque, radial force at the actual offset, allowable shock events and backlash acceptance conditions. A purpose-built planetary hub can be suitable for high wheel loads; a precision cycloidal reducer can be worth evaluating when low lost motion and overload capacity are priorities. Topology alone cannot approve either design.

This comparison is for AGV/AMR engineering teams and OEM buyers worldwide who have already chosen a geared drive. For the preceding architecture decision, see Direct Drive vs. Geared AGV Drive Wheels.

Scope and evidence — reviewed 2026-11-03: The equations and worked example below are reproducible screening calculations with stated assumptions, not measured hardware results or supplier approvals. Manufacturer pages support only the named product features; they do not establish universal shock multipliers, end-of-life backlash or docking precision. Local safety requirements and the exact supplier configuration still need review.

Preparing a shortlist? Send the wheel-load envelope and duty cycle for a technical RFQ, using the checklist below.


1. Why Wheel Loads Need More Than a Gearbox Torque Rating

A reducer coupled to an externally supported shaft sees a different load path from a gearbox that directly supports a wheel. Stationary machinery can also have severe loads; the key distinction is which bearings carry the forces. In a wheel-mounted drive, account for vehicle weight distribution, load transfer, tire compliance, turning scrub and floor impacts.

Cylindrical geared motor assembly with a projecting output shaft and mounting flange

Figure 1: Geared motor reference image. No wheel or tire is shown; the image does not establish internal gear topology or wheel-load capacity.

A. Overhung Radial Force and Tilting Moment

If a wheel is cantilevered from the gearbox, its radial load acts at an offset from the bearing support datum:

M_b = F_r * L_offset

For an assumed wheel load of 6,000 N and offset of 0.035 m, M_b = 210 Nm. Define the datum on a drawing: an offset from the mounting face is not automatically the offset from the outer bearing center. Internal bearing span and preload affect reactions and deflection.

B. Dynamic Shock Loads

A floor strike can load gear teeth, shafts, bearings and mounts. Step height, travel speed, tire stiffness, suspension, mass distribution and drivetrain compliance all influence the transient. There is no universal conversion from a 4 mm step to a torque multiplier. Record or model the transient and ask the supplier which torque limit applies to its duration and recurrence.

C. Reversals and Backlash

With motor-side feedback, reversal can produce encoder motion before the wheel responds. Output-side feedback can observe motion after the gearbox, but tire deformation and slip remain. Use a backlash and compliance budget appropriate to the actual navigation and docking system.


2. Planetary vs. Cycloidal Mechanics and Shock Capacity

The schematic illustrates different load paths. It is not a contact simulation, dimensioned design or overload rating.

Involute Planetary GearheadPrecision Cycloidal (RV) ReducerSun GearTooth Mesh ContactsCheck root bending + contact stress• Contact: Involute gear rolling + sliding• Load sharing depends on geometry• Shock limit: use model-specific ratingEccentric CamMultiple Pins Can Share LoadContact stress + bearing loads• Contact: Cycloidal lobes rolling over pins• Pin loading depends on clearances• Shock limit: use model-specific rating

A. Planetary Gearboxes: Tooth Bending and Contact Stress

A sun gear transmits torque through several planet gears and an internal ring gear. Tooth contact ratio and sharing between planets depend on tooth geometry, helix angle, tolerances, stiffness and alignment. Counting schematic contacts cannot establish shock capacity.

ISO 6336-3 provides a framework for spur/helical tooth bending assessment. A complete rating also needs the applicable contact-fatigue checks, material data, geometry and load factors. This guide does not reproduce a standards-compliant calculation or assign an application factor from floor geometry alone.

B. Cycloidal Reducers: Multiple Contacts, Model-Specific Limits

An eccentric mechanism drives lobed discs against a pin ring; some RV designs also use an initial involute stage. Several contacts can share load, but actual sharing depends on clearances and deformation. Contact fatigue, pins, eccentric bearings and output components can still limit the assembly.

For an example of published specifications, Nabtesco's product overview lists backlash and lost motion below 1 arcmin for RV-E models, while some right-angle models have different limits. This is a product specification, not evidence of unchanged backlash throughout service life or a universal 500% shock rating.


3. Cantilevered Overhung Loads and Output Bearing Architecture

A wheel-supporting gearbox needs a verified force-and-moment envelope as well as torque capacity. Check the complete hub, fasteners and chassis mounting interface.

AGV Drive Wheel Cantilevered Load Geometry & Moment ArmAMR CHASSISGearbox HousingBrg 1Brg 2Example Bearing DatumPolyurethane TreadØ 200 mm Wheel HubTire Contact CenterlineL_offset (e.g., 35 mm)F_r (Wheel Normal Load)M_b = F_r * L_offsetKey Overhung Load Metrics:• Normal load: F_r = m_wheel * g• Moment: M_b = F_r * L_offset• Bearing reactions depend on span• AGV hubs: check bearing arrangement• Cycloidal: verify main bearing option

Bearing Life Screening: What ISO 281 Does and Does Not Establish

First resolve wheel forces and moments into loads on each bearing using its arrangement and span. A simplified equivalent-load and basic-life calculation for a bearing is:

P = X * F_r_bearing + Y * F_a_bearing
L_10h = (10^6 / (60 * n)) * (C / P)^p
  • C is the bearing's basic dynamic load rating; P is its equivalent dynamic load, both in N.
  • X and Y come from the bearing manufacturer's method for that bearing and loading condition; they are not universal constants.
  • n is bearing relative speed in RPM for a constant-duty segment; p = 3 for ball bearings and 10/3 for roller bearings.
  • L_10h is basic rating life at 90% reliability under the method's assumptions. It is not the service life of the entire gearbox. Variable-duty loads require a suitable equivalent-load calculation; static indentation, lubrication, contamination, preload and shock need separate checks.

For a hypothetical two-support shaft with wheel load F_r = 4,000 N, overhang L = 40 mm beyond the outer bearing, and bearing span S = 30 mm:

Outer bearing reaction magnitude = F_r * (1 + L/S) = 9,333 N
Inner bearing reaction magnitude = F_r * L/S = 5,333 N (opposite direction)

This is a rigid, simply supported shaft example; it is not a model for every preloaded hub or crossed-roller bearing. It illustrates why quoting wheel force without its offset can hide the bearing demand. No failure date can be inferred without bearing data and duty history.

Purpose-Built Hubs and Integrated Main Bearings

Neugart's NGV documentation describes direct chassis mounting, an output bearing arrangement using preloaded angular contact roller bearings, and installation largely inside the wheel. This provides a counterexample to the idea that planetary gears are restricted to low wheel loads. Use the configured load limits at the actual datum, not a family-wide radial-force estimate.

Some cycloidal assemblies include a main bearing; others need additional support. Verify combined radial/axial/moment capacity and life for the exact product. Neither the gear topology nor the bearing name establishes an allowable wheel load.


4. Backlash, Odometry Drift, and Docking

A. Convert Output Backlash to Tangential Lost Motion

For an assumed output-side backlash angle, the corresponding wheel-rim displacement is:

delta_s = r_wheel * (theta_arcmin / 60) * (pi / 180)

The values below are calculated sensitivities, not typical specifications assigned to gearbox families. They assume a rigid wheel and full traversal of the stated angular gap.

Wheel diameterAssumed 12 arcminAssumed 3 arcminAssumed 1 arcmin
150 mm0.262 mm0.065 mm0.022 mm
200 mm0.349 mm0.087 mm0.029 mm
250 mm0.436 mm0.109 mm0.036 mm
300 mm0.524 mm0.131 mm0.044 mm
350 mm0.611 mm0.153 mm0.051 mm
400 mm0.698 mm0.175 mm0.058 mm

B. Differential Drive Heading Sensitivity

For track width B, ideal differential-drive kinematics gives:

delta_psi = (delta_s_right - delta_s_left) / B

If opposing wheel displacement errors are assumed to be +0.349 mm and -0.349 mm on a 600 mm track, the heading discrepancy magnitude is 0.698 / 600 = 0.00116 rad, or about 0.067 degrees. Sign depends on the yaw convention.

This single-event bound cannot predict accumulated drift over 100 reversals. Error signs, loading, tire slip, controller compensation and external pose updates matter. Validate docking performance on the complete vehicle rather than equating a gearbox backlash number with localization accuracy.

C. Specify Backlash Drift as an Acceptance Test

Request initial and post-endurance backlash or lost-motion results at the same torque, temperature, direction and output position. Define the duty cycle and permitted increase. Separate gear clearance from torsional compliance and bearing deflection. No universal 10,000-hour drift curve or lifetime zero-backlash guarantee follows from the topology.


5. Gearbox Comparison: What Buyers Must Verify

This 12-row matrix is a shortlist framework. It intentionally uses configuration-dependent checks instead of unsupported family-wide price, efficiency or life ranges.

Engineering parameterGeneral planetary gearheadPurpose-built AGV planetary hubPrecision cycloidal / RV assemblyRight-angle hypoid / bevel assembly
Load pathSun, planets and ring; wheel support may be externalPlanetary stage integrated with a wheel-support conceptEccentric discs and pins; RV may include a gear stageIntersecting or offset axes, depending on design
Load sharingDepends on tooth geometry and planet alignmentSame tooth checks plus hub stiffnessDepends on pin geometry, clearances and stiffnessDepends on tooth geometry and alignment
Shock capacityVerify repetitive and emergency torque separatelyVerify the same limits for the configured hubVerify permitted peak duration and event countVerify each stage and complete assembly
Initial backlashObtain output-side test conditionsObtain hub configuration and test conditionsLow-backlash models available; verify the chosen modelVerify complete train, including added stages
Backlash driftRequire endurance acceptance dataInclude hub bearings and wheel interfaceRequire endurance data; no lifetime assumptionInclude all stages in endurance testing
Wheel-load capacityCheck whether external support is neededCheck radial/axial force and moment envelopeConfirm main bearing inclusion and capacityConfirm wheel-bearing support arrangement
Reduction ratioCheck stage count and motor speedCheck available configured ratioCheck actual ratio and permitted input speedCheck total ratio across combined stages
EfficiencyRequest speed/load/temperature mapInclude hub seals and bearing lossesInclude eccentric mechanism and preload lossesHypoid sliding and bevel geometry differ
Breakaway and dragRequest no-load torque at operating temperatureInclude seals, grease and preloadRequest measured starting and running torqueInclude lubricant and mounting orientation
PackagingCheck motor length plus external bearingsCheck wheel-rim recess and motor envelopeCheck axial depth, diameter and adaptersCan relocate motor axis; check total envelope
Purchase costQuote matched rating and annual volumeInclude wheel, adapters and integrationInclude support bearings, adapters and serviceInclude extra stages and supports
Selection boundarySuitable if every load and duty limit passesCandidate when integrated wheel support helpsCandidate when specified lost-motion and load limits fitCandidate when motor orientation requires it

Before comparing quotes, review the integrated steering drive wheel interface against your CAD envelope and load datum.


6. Worked Sizing Example: A Hypothetical 2,000 kg AMR

This is an illustrative calculation, not a customer case, product selection or physical test. Its purpose is to turn a vehicle requirement into supplier-checkable outputs.

Assumed Operating Specification

  • Gross laden mass: 2,000 kg (500 kg chassis + 1,500 kg payload).
  • Two driven wheels share 65% of vehicle weight equally; other wheels carry the remainder. Load transfer is excluded from this first screen.
  • Wheel diameter: 250 mm; contact center is 35 mm beyond an explicitly defined outer-bearing datum.
  • Travel speed: 1.5 m/s; acceleration: 0.5 m/s^2; ramp: 3 degrees.
  • Rolling-resistance coefficient: assumed c_r = 0.02; gravity: 9.81 m/s^2.
  • A 25 mm joint with a 4 mm step is a test condition to report, not enough information to calculate impact torque.

Step 1: Wheel Output Speed and Torque

n_wheel = v * 60 / (pi * D) = 114.6 RPM
F_slope = m * g * sin(3 degrees) = 1,027 N
F_roll = m * g * cos(3 degrees) * 0.02 = 392 N
F_steady = 1,419 N
F_acc = m * a = 1,000 N
F_accelerating = 2,419 N
T_out_steady = (1,419 / 2) * 0.125 = 88.7 Nm per wheel
T_out_accelerating = (2,419 / 2) * 0.125 = 151.2 Nm per wheel

These values omit rotating inertia, turning scrub and drivetrain transients. The assumed driven-wheel normal load is about 6,377 N per wheel on level ground. Ignoring load transfer, the ramp acceleration demands a tire/floor friction coefficient of roughly 0.19; confirm traction under the actual floor condition.

Step 2: Gear Ratio and Motor Check

For an assumed motor rated at 3,000 RPM and 4.0 Nm, the speed-matching ratio is 3,000 / 114.6 = 26.18. At a candidate 25:1 ratio, the required motor speed is about 2,865 RPM. Using assumed efficiency eta = 0.93:

Available output at 4.0 Nm motor torque = 4.0 * 25 * 0.93 = 93.0 Nm
Required motor torque for acceleration = 151.2 / (25 * 0.93) = 6.50 Nm

The simple steady-torque balance is positive, with only about 5% margin. This does not establish thermal suitability. Verify the motor's torque-speed curve, acceleration duration, RMS heating, voltage/current limits and the gearbox's own torque rating. The assumed efficiency is not a catalog claim.

Step 3: Shock Sensitivity, Not a Floor-Impact Prediction

As an unvalidated sensitivity assumption, apply a multiplier of 3.5 to the rounded steady output torque:

T_sensitivity = 88.7 * 3.5 = 310.5 Nm per gearbox

This value is not derived from the 4 mm step or assigned by ISO. If measurements or a validated model establish this demand, a candidate must permit it at the relevant speed, duration and number of events. An emergency torque limit for a few stops does not establish suitability for repeated floor joints. No named planetary or cycloidal model is approved by this example.

Step 4: Wheel Load and Overhung Moment

F_r = 2,000 * 9.81 * 0.65 / 2 = 6,376.5 N per wheel
M_b = 6,376.5 * 0.035 = 223.2 Nm

Send the supplier this force, datum and moment together with axial loads and the loaded/unloaded duty cycle. Request combined-load capacity, bearing reactions, static safety and fatigue-life calculations. The result remains pending until the configured gearbox and wheel assembly are checked; a nominal torque or family load rating cannot provide a pass.


7. Engineering Decision Framework

  1. Resolve the load path: Does the gearbox support the wheel directly, or do separate bearings carry it? Record F_r, F_a, moment and drawing datum.
  2. Check envelope and speed: Compare motor orientation, installed wheel diameter, ratio and allowable input speed. A right-angle stage is an option when the envelope calls for it, not a chassis-height rule.
  3. Check the load spectrum: Compare continuous/RMS duty, acceleration, braking and measured or modeled impacts against the correct supplier limits.
  4. Set a motion-error budget: Choose backlash, lost-motion and stiffness acceptance criteria based on feedback placement and vehicle testing. Request endurance evidence for drift.
  5. Compare complete assemblies: Shortlist planetary hubs and cycloidal assemblies that meet those checks, then compare loss maps, cooling, service, lead time and installed cost.

A heavy vehicle does not automatically require cycloidal reduction, and a low backlash specification does not guarantee sub-millimeter docking. Keep both architectures in the shortlist when their configured ratings fit.


8. OEM Procurement and Engineering RFQ Checklist

Use this checklist to replace a vague request for a "1 kW 25:1 gearbox" with a reviewable specification.

  • Wheel forces and datum: Provide loaded/unloaded radial forces, axial forces, dynamic load transfer, offsets and a drawing identifying mounting and bearing reference planes.
  • Torque and speed spectrum: State continuous, acceleration, braking and impact output torque, motor input speed, duration and event counts. Mark unknown transients for measurement.
  • Bearing-life target: State the required hours and reliability; request a bearing calculation with duty assumptions plus static, shock and lubrication checks. Do not use L_10h as whole-gearbox life.
  • Backlash and stiffness acceptance: Specify output-side backlash/lost-motion limits, test torque and temperature, and post-endurance acceptance under the same method.
  • Motor and mechanical interface: Include torque-speed curve, peak duration, flange, shaft connection, hub bolt pattern and available CAD envelope.
  • Environment and sealing: State dust, water jets, immersion, cleaning chemicals and temperatures. Confirm assembly-level protection; IP67 immersion protection alone does not establish washdown suitability.
  • Lubrication and maintenance: Request permitted lubricant, mounting orientation, temperature range, relubrication interval and storage limits. Verify any lifetime-lubrication claim against the stated duty.
  • Stopping duty and system verification: Supply stop torque, stopping profile and expected counts. ISO 3691-4:2023 addresses driverless-truck safety and verification; a gearbox rating alone does not establish vehicle compliance.
  • Commercial evidence: Request a matched quotation, configuration drawing, exclusions, lead time, prototype availability and acceptance-test records.

9. Frequently Asked Questions

Can a standard planetary gearbox support an AGV drive wheel directly?

Only if its output bearings, shaft or flange, and mounting interface are rated for the actual wheel forces and moment at the stated load offset. A torque rating alone does not establish wheel-load capacity. An external bearing arrangement or a purpose-built wheel hub may be needed; bearing type alone is not an approval criterion.

Does a cycloidal reducer always withstand 500% shock torque?

No. Some products advertise high momentary overload capacity, but the permitted torque, duration, speed and event count are model-specific. Repeated floor impacts must be checked against the repetitive-duty limit. Neither planetary nor cycloidal construction guarantees freedom from fracture or bearing damage.

How does gearbox backlash affect AMR odometry and docking?

With a motor-side encoder, backlash allows motor rotation during reversal before corresponding wheel rotation occurs. At a 100 mm wheel radius, an assumed 12 arcmin output backlash corresponds to 0.349 mm of tangential lost motion. This is a geometric sensitivity estimate, not a docking accuracy guarantee; tire slip, compliance, feedback placement and sensor fusion also matter.

What are the main cycloidal versus planetary sourcing trade-offs?

Compare the actual ratio, continuous and repetitive peak torque, bearing-load envelope, backlash test method, part-load loss map, motor speed and installed dimensions. Precision cycloidal models can offer low backlash and integrated main bearings; AGV planetary hubs can also carry high radial loads. Obtain matched quotes and endurance data instead of applying a universal price or lifetime multiplier.

When should an AMR use a right-angle gearbox?

Consider a right-angle input when the motor and chassis envelope require it. Hypoid and bevel gears are different mechanisms and can be combined with other reduction stages. Confirm installed height, ratio, efficiency, thermal duty, lubrication and wheel-bearing support for the selected assembly.

What must an AGV drive wheel gearbox RFQ include?

Include loaded and unloaded wheel forces, load offset and datum, continuous and peak output torque, speed and duty cycle, impact and braking event duration and count, bearing-life target, backlash acceptance method, motor interface, operating environment and lubrication requirements. Ask the supplier to state assumptions and exclusions for the exact configuration.


Engineering Next Steps

Shortlist gearboxes by the actual torque, force-and-moment envelope, motion-error budget and operating duty. Use the worked example to structure the inputs, then replace its assumptions with your vehicle data and supplier limits.


Sources and Technical References

Sources were checked on 2026-11-03. These are manufacturer specifications and a public standards abstract, not independent endurance tests. ISO 6336-3 and ISO 281 are identified above as calculation frameworks; their full requirements have not been reproduced or verified here.

  1. Neugart NGV — Application-specific planetary gearbox. Supports the discussion of direct chassis mounting, wheel packaging and the specialized output-bearing concept. Use configuration-specific technical data for numerical selection.
  2. Nabtesco Motion Control — High precision cycloidal gears and product overview. Lists model-specific backlash/lost-motion specifications and main-bearing features. Does not establish a universal lifetime backlash or shock-torque guarantee.
  3. ISO 3691-4:2023 — Driverless industrial trucks and their systems. Public abstract identifies the safety and verification scope. It does not validate the assumed shock multiplier, gearbox life or a universal stopping-event count.

Author

avatar for Julian Thorne - Lead Robotics & Joint Actuator Architect
Julian Thorne - Lead Robotics & Joint Actuator Architect

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