New spec
Propulsionmediumgeneral

Pilotix 3115 900KV Brushless Motor with Plastic Pipes and Plug

A compact 3115-size brushless motor rated at 900KV, designed for medium-to-heavy-lift drones and commercial applications. Features protective plastic cable tubing and a pre-installed quick-disconnect high-current plug for rapid field replacement. Rated for 3–6S LiPo systems with up to 1592W peak power and 4080g maximum thrust.

EU localization
3/10
Per unit
€40–70
Starter batch
4units
To first batch
16weeks
Budget
€45,000–62,000 (€15k–20k NRE for tooling and winding fixtures; €25k–35k for 500-unit pilot batch at €50–65/unit; €5k–7k for testing, compliance, and logistics)

Bottom line

Brushless motor manufacturing is highly localized in Portugal through Allied Motion Portugal (motor assemblies) and EFACEC (copper winding/magnetics). Combined with Simoldes' injection molding for protective housings and Yazaki Saltano's wire harness capabilities, a fully local supply chain is viable. The 900KV rating and 12N/14P winding are non-standard, discouraging off-the-shelf white-label; co-development ensures the stator laminations, magnet strength, and balancing meet the 4080g thrust spec. China remains the price floor but adds 8–10 weeks shipping, tariff exposure, and field-testing risk.

Read full insight

Brushless motor manufacturing is highly localized in Portugal through Allied Motion Portugal (motor assemblies) and EFACEC (copper winding/magnetics). Combined with Simoldes' injection molding for protective housings and Yazaki Saltano's wire harness capabilities, a fully local supply chain is viable. The 900KV rating and 12N/14P winding are non-standard, discouraging off-the-shelf white-label; co-development ensures the stator laminations, magnet strength, and balancing meet the 4080g thrust spec. China remains the price floor but adds 8–10 weeks shipping, tariff exposure, and field-testing risk.

What it does

Converts electrical energy from the battery into rotational motion to spin the propeller

Provides up to 4080g of thrust for lifting the drone and payload

Enables quick motor replacement in the field via a plug-in connector without soldering

How it's made

  1. 1

    Wind stator coils

    12-pole copper wire wound onto laminated silicon-steel stator core

  2. 2

    Machine rotor bell and shaft

    CNC-turn aluminum bell and steel shaft; press neodymium magnets into bell

  3. 3

    Assemble and balance

    Fit double bearings, mount rotor, dynamically balance the rotating assembly

  4. 4

    Solder and protect wiring

    Attach silicone leads, thread through protective plastic tubing, crimp connector

  5. 5

    Test and inspect

    Spin-test under load, verify KV, resistance, and vibration; apply final QC labels

Risks to watch

  • Neodymium magnet supply and price volatilityhigh

    High-grade N52 neodymium magnets are critical for achieving 4080g thrust and the 900KV rating. Europe has minimal domestic production; most magnets are imported from China (Ningbo, Ganzhou). Rare-earth price spikes (2021–2022 saw 40% increases) or export restrictions can delay production and inflate costs. Portuguese motor assemblers typically hold 4–6 weeks of magnet inventory, creating a bottleneck if lead times extend.

    → Mitigation: Dual-source magnets from Vacuumschmelze (Germany) and Arnold Magnetic (UK/Czechia) in addition to Chinese suppliers. Negotiate 12-week supply agreements with price caps. Design the rotor to accept N48–N52 magnets (slightly different field strengths) so the winding can be re-tuned if supply constraints force a grade swap. Stock 3 months of safety inventory once the design is validated.

  • Intellectual property leakage on custom 12N/14P windingmedium

    The 12N/14P winding configuration and the precise turn count to achieve 900KV ±5% are proprietary. If drawings or winding specs are shared with multiple vendors (especially during prototyping), a less scrupulous partner or subcontractor could replicate the design for a competitor or gray-market clone. This is a particular concern if Chinese factories are used for cost-down pressure in later production phases.

    → Mitigation: File a Portuguese utility model or EU design right on the stator winding pattern before distributing CAD files. Use NDAs with penalty clauses tied to revenue loss. For local production, Allied Motion Portugal has aerospace-grade IP controls (ITAR-adjacent practices). Watermark technical drawings with unique serial codes. Manufacture stators and rotors at separate facilities, final assembly only at a secure site.

  • CE and Radio Equipment Directive (RED) electromagnetic interferencemedium

    Brushless motors generate significant EMI, especially at 63.7A peak current. If the motor interferes with the drone's 2.4GHz or 5.8GHz radio links, the entire UAV may fail RED compliance testing (EN 301 489). Many Chinese motors lack proper EMI shielding and filtering. Even EU-manufactured motors require testing in the final drone assembly; a late failure after 500 units are built would require expensive rework (ferrite rings, shielded wiring, capacitor banks).

    → Mitigation: Specify EMI suppression in the motor contract: include 100nF ceramic capacitors across each phase winding and ferrite beads on the silicone leads. Conduct pre-compliance EMI scanning with a spectrum analyzer at Allied Motion Portugal before committing to full production. Budget €5,000 for notified-body RED testing of motor + ESC + flight controller as a subsystem. Design the plastic tubing with carbon-loaded plastic (from Composites Kingdom) for mild RF shielding if early tests show issues.

  • Extended lead time for Japanese anti-corrosion bearingsmedium

    The spec calls for double Japanese bearings with anti-corrosion coating (likely NSK or NTN with zinc-chromate or ceramic hybrid balls). These bearings typically have 8–12 week lead times from Japan, and COVID-era supply chain disruptions occasionally extend this to 16 weeks. If Allied Motion Portugal or the rotor machining partner runs out of bearing stock mid-production, motor assembly halts.

    → Mitigation: Pre-order 6 months of bearing inventory (2,000–3,000 units) once the shaft diameter (5mm) is frozen. Qualify a European alternative such as SKF (Sweden) stainless-steel bearings with PTFE seals (longer lead time but EU-sourced). Design the rotor bell bore with ±0.01mm tolerance so both NSK and SKF bearings fit without retooling. Use a postponement strategy: build and stock rotor bells and stators separately, final bearing press and assembly only when customer orders confirm.

  • Dynamic balancing failures leading to vibration and thrust losshigh

    Achieving 4080g thrust at 900KV requires the rotor assembly to be dynamically balanced to <0.5g·mm residual imbalance. Poor balancing causes vibration, accelerated bearing wear, and reduced flight time. Automated balancing machines are expensive (€40,000–80,000); smaller contract manufacturers may use manual balancing, which is operator-dependent and inconsistent. A batch of 500 motors with 10% out-of-balance units would trigger costly field replacements and damage Pilotix's reputation.

    → Mitigation: Require Allied Motion Portugal or the final assembler to use a Schenck or CEMB two-plane dynamic balancing machine with ISO 21940 certification. Include a 100% inline balance check (15 seconds per motor) in the production line; reject any unit >0.5g·mm. Perform incoming inspection of rotor bells from Hypermetal/Engenhotec for runout <0.02mm before magnet insertion. Run a 30-unit pilot batch with full vibration spectrum analysis (accelerometer on motor mount) to validate the balancing process before scaling to 500+ units.

Production timeline

16 weeks · 7 steps

Step-by-step plan7

Full description of every production step

  1. 1

    Design freeze and tooling preparation

    3w

    Finalize CAD models for the stator lamination stack, rotor bell geometry, and shaft dimensions. Generate winding schematics (12N/14P, 900KV target) and magnet placement drawings. Allied Motion Portugal and Hypermetal review for DFM. Order stator lamination punch tooling (€8,000–12,000), rotor bell CNC programs, and injection molds for plastic tubing end-caps from Simoldes. Procure neodymium magnets (N52, arc segment) and Japanese bearings (NSK/NTN) with 10-week lead time.

  2. 2

    Stator core lamination and winding

    4w

    Punch silicon-steel laminations (0.35mm thickness) and stack into 12-slot stator cores at EFACEC or Allied Motion's winding facility. Wind copper wire (AWG 18–20) onto each tooth using automated needle winders to achieve 900KV rating. Insulate with polyimide tape and epoxy-impregnate for thermal stability (Class H, 180°C). Cure in oven for 4 hours. Test resistance and inductance on each phase; reject units outside ±3% tolerance. Output: 550 stator assemblies (including 10% spares).

    Needs: Design freeze and tooling preparation

  3. 3

    Rotor bell and shaft machining

    3.5w

    CNC-turn 6061-T6 aluminum rotor bells (31mm OD, 15mm height) and harden-steel motor shafts (5mm diameter, M3 tapped prop-mount holes) at Hypermetal or Engenhotec. Anodize rotor bells for corrosion resistance. Press-fit neodymium magnets into the bell inner surface using an alignment jig to ensure even spacing (14 poles). Drill and ream shaft bore to H7 tolerance. Press shaft into bell with Loctite 648. Inspect magnet alignment with a Hall-effect probe; reject any bell with >2° pole skew.

    Needs: Design freeze and tooling preparation

  4. 4

    Bearing installation and rotor-stator assembly

    2.5w

    Press double Japanese bearings (5×10×4mm, shielded with anti-corrosion coating) into stator end-bells using a thermal press (heating bearing outer race to 80°C). Insert rotor shaft through bearings and secure with snap rings. Check axial play (<0.1mm) and radial runout (<0.02mm). Mount stator onto assembly base plate with M3 screws. Dynamically balance the rotor assembly on a two-plane balancing machine (Schenck); remove material from rotor bell fins to achieve <0.5g·mm residual imbalance. Re-check after balancing.

    Needs: Stator core lamination and winding, Rotor bell and shaft machining

  5. 5

    Wire harness assembly and connector installation

    1.5w

    Solder 14 AWG silicone motor leads (red/black/yellow for phases A/B/C) to stator phase terminals. Thread wires through protective plastic tubing (injection-molded by Simoldes, 4mm ID, flame-retardant PA12). Crimp MT60 or XT60 male connector pins onto wire ends at Yazaki Saltano's harness line. Insert pins into connector housing and secure with locking tabs. Apply heat-shrink tubing over solder joints. Perform 100% pull-test (5kg load, 10 seconds) and hi-pot test (500V DC, 1 second) to verify insulation integrity.

    Needs: Bearing installation and rotor-stator assembly

  6. 6

    Electrical and mechanical testing

    1w

    Spin each motor on a dynamometer test stand at 50%, 75%, and 100% throttle with a 6S LiPo pack and appropriate propeller (15×5.5 or 16×5.5). Measure KV (rpm/volt) with optical tachometer; target 900 ±45 rpm/V. Record internal resistance (3-phase line-to-line, target ≤0.046Ω), peak current (should handle 63.7A for 60s without thermal shutdown), and thrust (verify ≥4080g at full throttle). Check vibration with accelerometer; reject units >0.3g RMS. Log serial number and test data in MES (Critical Manufacturing or similar).

    Needs: Wire harness assembly and connector installation

  7. 7

    Final QC, labeling, and packaging

    0.5w

    Visual inspect for scratches, magnet chips, and connector damage. Apply laser-engraved serial number and CE/RoHS compliance label to motor base. Package each motor in ESD-safe foam insert within a printed cardboard box (sourced from local packaging supplier). Include quick-start guide (motor specs, prop recommendations, ESC settings) and compliance declaration. Palletize in sets of 50 motors. Conduct final audit on 5% of batch per ISO 2859 AQL 1.5. Release to Pilotix warehouse in Lisbon.

    Needs: Electrical and mechanical testing

  1. 1Design freeze and tooling preparation· 3w
  2. 2Stator core lamination and winding· 4w
  3. 3Rotor bell and shaft machining· 3.5w
  4. 4Bearing installation and rotor-stator assembly· 2.5w
  5. 5Wire harness assembly and connector installation· 1.5w
  6. 6Electrical and mechanical testing· 1w
  7. 7Final QC, labeling, and packaging· 0.5w
Technical specs

5 processes · 6 materials · 8 parts

Processes

Motor WindingCNC MachiningInjection MoldingWire Harness AssemblyTesting & Inspection

Materials

copper wire

copper wire

silicon steel laminations

silicon steel laminations

neodymium magnets

neodymium magnets

aluminum alloy

aluminum alloy

plastic tubing

plastic tubing

silicone wire

silicone wire

Key requirements

  • 12N/14P winding configuration
  • 900KV rating ±5%
  • internal resistance ≤0.046Ω
  • 5mm shaft diameter with 4×M3 prop mount holes
  • peak current handling 63.7A for 60s
  • double Japanese bearings with anti-corrosion coating
  • IP54-equivalent dust and moisture resistance
  • pre-installed MT60 or equivalent high-current connector

Bill of materials

  • 1
    Stator assembly
  • 2
    Rotor bell and magnets
  • 3
    Motor shaft
  • 4
    Double bearing set
  • 5
    Silicone motor wires
  • 6
    Protective plastic tubing
  • 7
    Pre installed connector plug
  • 8
    Mounting screws
Compliance checklist9

Regulations and certifications to clear

  • CE marking under Low Voltage Directive 2014/35/EU (motor operates 22.2–25.2V, technically exempt but mark for market access)
  • RoHS Directive 2011/65/EU (lead-free solder, compliant neodymium magnet coatings)
  • REACH Regulation (EC) 1907/2006 (SVHC declaration for neodymium, copper, aluminum)
  • Radio Equipment Directive (RED) 2014/53/EU EMC requirements EN 301 489-1/-3 (EMI from brushless commutation)
  • Machinery Directive 2006/42/EC if sold as stand-alone; safety risk assessment for rotating parts
  • EASA Easy Access Rules for Unmanned Aircraft Systems (UAS) Part 1-4 if integrated into >25kg MTOW drone
  • IEC 60529 IP54 rating validation (dust and splash resistance for motor housing)
  • ISO 21940 dynamic balancing certification (vibration limits for rotating machinery)
  • EU Dual-Use Regulation 2021/821 (export control if thrust >500N or used in >25kg UAS—not applicable here but monitor)