NuiCent M4 — The Invention
NuiCent Gen by Will Cole
NuiCent M4 — The Invention
A four-arm experimental mechanical prototype using two counter-running GT2 main loops, moving sliders, Positive Locks, a floating N20 centre drive and interchangeable higher-power 5065 or lightweight 31YZ gyro / generator modules.
Motor options • How it works • Engineering data • Free download
Applications & Development Paths
The same four-arm NuiCent core can be packaged around different gyro/generator sizes. The applications below are experimental development directions and require prototype testing for each installation.
Self-Balancing Unicycle
Compact low-mounted four-arm core between two close wheels, with automatic fore/aft pitch balancing, one traction motor per wheel and rider-controlled left/right steering.
Perpetual Aviation / UAV & eVTOL R&D
Balanced counter-rotating gyro research, attitude-control experiments and auxiliary electrical-power studies for unmanned and electric aircraft concepts.
Marine Propulsion
Experimental hybrid marine layouts for auxiliary generation, pumps, controls, battery support and mechanically assisted propulsion studies.
Electric Vehicles
Range-extension research, auxiliary electrical power, kinetic buffering and regenerative test systems for cars, bikes, vans and other EV platforms.
Off-Grid & Remote Power
Battery/capacitor charging research, remote-site test systems and mechanically driven auxiliary generation where a measured input source is available.
Industrial Machinery
Auxiliary-power, rotating-inertia, peak-load buffering and machinery-assist experiments.
HVAC / Air Conditioning
Research into mechanically assisting compressor/fan systems and recovering useful electrical power from externally driven rotation.
Energy Storage & Buffering
Rotational-energy, battery and capacitor buffering experiments for transient loads, charging systems and DC-bus support.
Choose Your Motor Configuration
The same NuiCent M4 core can be developed around two very different generator/gyro packages: the higher-power 5065 concept or the lighter 31YZ small-drone configuration.
16 × 5065 — Higher Power
Layout: 4 motors per arm × 4 arms
Representative motor mass: ~480 g each
Bare motor mass: ~7.68 kg total
NuiCent design target: ~500–1,000 W electrical per unit, ~8–16 kW total*
Holder: dedicated larger 5065 holder replacing the 31YZ holder
Best suited to: larger UAV/eVTOL research, marine/vehicle auxiliary generation, industrial and off-grid experimental systems.
16 × 31YZ — Lightweight Drone
Layout: 4 motors per arm × 4 arms
Motor mass: ~160 g each
Bare motor mass: ~2.56 kg total
31YZ output target: 240 W combined from 16 units — 15 W per 31YZ*
Baseline: 12 V / ~3500 rpm project reference
Best suited to: small UAV research, avionics/telemetry auxiliary power, lightweight gyro-control, battery/capacitor buffering and test platforms.
*Both figures are engineering targets/test ranges, not guaranteed continuous output. Real ratings require loaded voltage/current, torque, temperature and mechanical-input measurements on the actual motors and finished transmission.
Watch the M4 motion cycle
This animated demonstration shows the corrected M4 motion and Positive Lock handover cycle from the current CAD sequence.
How NuiCent M4 works
The M4 is a four-quadrant radial mechanism. Two independent 3600 mm GT2 belts follow the same XY route on two separate Z-levels and counter-run through the centre. As the slider geometry moves, belt length is redistributed through multiple moving spans, creating the double-pull transfer between opposite arms.
At each 90° state change, the arriving inner slider releases the previously locked neighbouring state and then captures its own central position using the Positive Lock / wedge system. The sequence is mechanical rather than based on a programmed handover delay.
Main mechanical groups
- Four-arm rail and slider system: guides radial travel and the 90° handover sequence.
- Positive Locks and wedges: hold the active central position and coordinate release/capture.
- Two 3600 mm GT2 main loops: transmit the main give/take movement between opposing arms.
- Local GT2 stages: four 466 mm, four 200 mm and four 176 mm closed loops.
- Floating N20 centre drive: four guide locations let the centre move without making the N20 shaft the structural hinge.
- T70 one-way freewheel: allows overrun/free-spin when the driven centre is moving faster than the N20 drive.
- Dedicated 5065 holder system: the higher-power configuration replaces the small 31YZ holders with 5065-class motor/generator holders sized for the larger 50 × 65 mm motor envelope. The lighter 31YZ configuration remains a separate small-drone option.
Current M4 engineering data
| Main belts | 2 × 3600 mm GT2, counter-running |
| Total GT2 loops | 14 |
| Local loops | 4 × 466 mm, 4 × 200 mm, 4 × 176 mm |
| Main route planes | Z = +38.0 mm and Z = −24.0 mm |
| Plane separation | 62.0 mm |
| Opposite-slider travel | 63.72 mm design value |
| Nominal belt transfer / 90° | 764.64 mm per main loop (calculated target) |
| Combined loop movement / 90° | 1529.28 mm calculated target |
| Practical swing target | about 22–23° |
| N20 guide/bearing pockets | 16.1 mm |
Calculated transfer figures are design targets. Final belt movement, shaft speed, tension and endurance must be measured on the printed prototype.
Balanced 2 + 2 gyro arrangement
The preferred configuration uses two matched clockwise and two matched counter-clockwise rotating modules, all labelled from the same viewing side. This reduces the net stored angular momentum seen by the frame when the pairs are well matched while still allowing coordinated tilt/control torques to be produced by commanding the paired tilt directions appropriately.
Two gyro drives are allocated to MAIN 1 and two to MAIN 2 so the two 3600 mm belts share the drive load instead of concentrating it on a single loop.
Self-Balancing Unicycle Development
The compact NuiCent layout is also being developed for a two-close-wheel self-balancing unicycle. The intention is to mount the four-arm gyro core low between the wheels so fore/aft pitch can be actively stabilised while the rider retains natural left/right control through body and knee input.
Mechanical Layout
- Two closely spaced wheels.
- One traction motor per wheel for symmetric drive.
- NuiCent core positioned low between the wheels.
- Four radial arms with balanced counter-rotating gyro groups.
- Compact rails, inner/outer sliders, idlers and Positive Locks retained from the M4 development.
Intended Function
- Automatic forward/back pitch balancing.
- Rider-controlled left/right balance and steering.
- Gyro-control research with the preferred 2 + 2 counter-rotating arrangement.
- Auxiliary generation and battery/capacitor buffering experiments.
- Compact personal-mobility research platform.
This is an experimental prototype concept, not a certified road vehicle. Stability, braking, electrical output, mechanical endurance and rider safety require physical testing before use.
16 × 5065 higher-power configuration
The higher-power NuiCent concept replaces the 31YZ motor holders with dedicated 5065 holders, arranged as four 5065-class motor/generator units per arm for 16 units total. A representative Racerstar 5065 140KV unit is listed at about 480 g and up to 1,200 W motor power; the exact motors fitted to NuiCent must still be weighed and bench-tested individually.
Using 480 g as the planning mass gives approximately 7.68 kg of bare 5065 motor mass for sixteen units before holders, shafts, pulleys, bearings, fasteners and wiring.
| Design target / 5065 | 16-unit electrical total | Illustrative generator mechanical input at 85%* |
|---|---|---|
| 500 W | 8 kW | ≈9.41 kW |
| 750 W | 12 kW | ≈14.12 kW |
| 1,000 W | 16 kW | ≈18.82 kW |
*These are design/output targets, not measured NuiCent ratings. Mechanical input must be greater than electrical output once generator, belt, bearing, lock and conversion losses are included. A 5065 size/KV label does not by itself establish a safe continuous generator rating.
Perpetual Aviation — proposed 5065 applications
- Large UAV / eVTOL research: higher-power gyro and generation experiments with balanced counter-rotating groups.
- Auxiliary electrical power: avionics, pumps, fans, sensors, lighting and battery/DC-bus charging from externally supplied mechanical power.
- Regenerative research: recovering part of stored rotational energy during controlled deceleration where the drive and electronics are designed to back-drive.
- Hybrid power buffering: using rotating inertia alongside batteries or capacitors to smooth transient loads.
- Attitude-control research: coordinated counter-rotating gyro pairs for experimental pitch, roll and yaw torque control.
16 × 31YZ lightweight small-drone configuration
For smaller Perpetual Aviation drone research, the M4 can retain 16 × 31YZ / 31ZY permanent-magnet units, four per arm. At approximately 160 g per motor, the sixteen bare motors total about 2.56 kg before carriers, pulleys, bearings, belts, wiring and guards — roughly one-third of the bare-motor mass of the representative 16 × 5065 set.
The 12 V / 3500 rpm project baseline gives roughly 12 V open circuit near 3500 rpm, but usable watts depend on loaded current and temperature. Until one actual 31YZ is bench-tested, the safest way to present output is as a measured-current table:
| Loaded current / 31YZ at 12 V | Electrical / motor | 16-motor total |
|---|---|---|
| 0.10 A | 1.2 W | 19.2 W |
| 0.25 A | 3.0 W | 48 W |
| 0.50 A | 6.0 W | 96 W |
| 0.75 A | 9.0 W | 144 W |
| 1.00 A | 12.0 W | 192 W |
| 1.25 A | 15.0 W | 240 W target |
The NuiCent 31YZ configuration uses a 240 W combined electrical output target for sixteen units, equivalent to 15 W per 31YZ. At 12 V that corresponds to approximately 1.25 A per motor under load. This remains a design target until the exact 31YZ units demonstrate the required loaded current continuously without excessive brush, winding or commutator temperature.
Small Perpetual Aviation drone uses
- Avionics, flight-controller and sensor supply.
- Navigation lights, communications and telemetry.
- Battery/capacitor buffering and in-flight auxiliary charging experiments.
- Counter-rotating gyro attitude-control experiments using the preferred balanced arrangement.
- Regenerative and load-smoothing research on small UAV test platforms.
The 31YZ configuration is an experimental auxiliary-power and gyro-control concept. It is not evidence of perpetual flight, and its electrical output cannot replace the energy required by the propulsion motors without an external source and a measured energy balance.
Lock-cycle and wear data
The M4 changes state four times per centre revolution. Each individual inner slider completes two full lock-release cycles per centre revolution. Across all four sliders there are eight lock engagements and eight releases per revolution.
| Centre RPM | Cycles / inner slider / hour | All-system engagements / hour |
|---|---|---|
| 52 | 6,240 | 24,960 |
| 60 | 7,200 | 28,800 |
| 90 | 10,800 | 43,200 |
| 120 | 14,400 | 57,600 |
This makes the wedge faces, slider noses, pivot bores, stops and belt-contact surfaces key endurance-test items.
Radial loading reference
Using four 31YZ units at approximately 160 g each gives a 0.64 kg bare-motor carrier mass before printed parts, bearings, pulleys, fasteners and wiring. At the current outward reference radius, the bare-motor radial load is approximately 3.89 N at 52 rpm, 5.18 N at 60 rpm, 11.66 N at 90 rpm and 20.74 N at 120 rpm.
These are carrier radial-load calculations, not direct belt-tension measurements. The actual belt load depends on the complete moving mass, pulley geometry, loaded spans, friction and generator torque.
Free 3D-printable N20 / GT2 mount
The free-spinning N20/GT2 direct-drive mount was developed for the NuiCent centre drive. It uses a four-hole direct-drive interface and an overrun/free-spin arrangement intended to reduce rigid load transfer back through the small N20 shaft and gearbox.
Download the free STEP + STL motor mount →
Prototype status and testing
NuiCent M4 is an experimental mechanical R&D prototype. The finished CAD defines the intended geometry and motion sequence, but the automatic lock/release cycle, endurance life, loaded shaft speeds, belt tension and overall input/output performance require physical bench validation.
Any electrical output from 31YZ units is conversion of mechanical/electrical input and stored rotational energy. Input power and output power must be measured independently when assessing efficiency. The NuiCent name does not by itself establish perpetual-motion or over-unity performance.
Safety: high-speed rotating parts, belts and locking components must be operated behind a rigid guard, with current-limited first tests and an emergency stop.
Invented and developed by Will Cole
NuiCent Gen • M4 FinishedNew development • 2026