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MF2614VP

By T-MOTOR ↗

The T-MOTOR MF2614VP is a 26.4inch folding, manual variable-pitch propeller for multirotor and VTOL aircraft. Replaceable positioning blocks adjust pitch for different operating conditions. Polymer+CF construction, recommended motor and ESC pairings, and conditional selection tables define its integration parameters; higher-angle configurations carry explicit restrictions.

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Model and applicationT-MOTOR MF2614VP manual variable-pitch propeller for multirotor and VTOL aircraft
ArchitectureFolding
Weight142.6gSingle blade.
Package weight457.6gPackaged product.
Diameter26.4inch (670.56mm)
Package size334*134*61mmPackaged product.

Product overview

The T-MOTOR MF2614VP is a folding, manual variable-pitch propeller for multirotor and VTOL aircraft. Its positioning blocks allow manual pitch changes for different flight speeds, altitudes and aircraft weights. Polymer+CF construction, a 26.4inch (670.56mm) diameter and a 142.6g single-blade weight define its physical configuration. Recommended integration equipment comprises the MN805S KV170/KV150 motor and FLAME 180A 12S V2.0 ESC. Recommended thrust is 3~8kg, with a recommended maximum of 18.5kg. Package dimensions are 334*134*61mm and package weight is 457.6g.

The specified pitch is 9.4inch (238.76mm); the separate positioning-block reference maps 0°, 2.5°, 5°, 7.5° and 10° blocks to 9.1, 11.9, 14.7, 17.6 and 20.6inch respectively. Speed-based selection applies at 0~2000m altitude, while altitude-based selection applies below 15m/s. Both references mark 7.5° and 10° as not recommended. These blocks and other angles are available through customization upon request. Standard customization has MOQ 1 and permits pitch angles specified to 0.01°; assisted mass-production customization can fix the selected pitch before shipment.

Ambient temperature limits are -40°C to 65°C, with storage at -10°C to 50°C and humidity below 85%. The MN805 KV170 bench configurations carry burnout warnings at +2.5° and +5°, and discourage static testing at +7.5° and +10°. Cover-plate screws must be secure, and propellers damaged by a fall or equivalent impact require replacement. The propellers must not be disassembled or used in the specified chemically hostile environments. Storage beyond six months requires sealed preservation.

Specifications

SpecificationValue & conditions
Model and applicationT-MOTOR MF2614VP manual variable-pitch propeller for multirotor and VTOL aircraft
ArchitectureFolding
Weight142.6gSingle blade.
Package weight457.6gPackaged product.
Diameter26.4inch (670.56mm)
Package size334*134*61mmPackaged product.
Pitch9.4inch (238.76mm)
MaterialPolymer+CF
Recommended thrust3~8kg
Recommended maximum thrust18.5kg
Ambient temperature-40°C to 65°C
Storage temperature and humidity-10°C to 50°C / less than 85%Storage.
Recommended ESCFLAME 180A 12S V2.0
Recommended motorMN805S KV170/KV150
Positioning-block selection by flight speed
  • 0~10m/s: 0°;
  • 5~15m/s: 2.5°;
  • 10~20m/s: 5°;
  • 15~25m/s: 7.5° (not recommended);
  • 20~30m/s: 10° (not recommended)
Flight altitude 0~2000m.
Positioning-block selection by flight altitude
  • 0~1000m: 0°;
  • 0~2000m: 2.5°;
  • 0~3000m: 5°;
  • 1000~4000m: 7.5° (not recommended);
  • 2000~5000m: 10° (not recommended)
Flight speed below 15m/s.
Pitch by positioning block
  • 0°: 9.1inch;
  • 2.5°: 11.9inch;
  • 5°: 14.7inch;
  • 7.5°: 17.6inch (not recommended);
  • 10°: 20.6inch (not recommended)
Pitch adjustmentManual replacement of positioning blocks
Additional positioning blocks7.5°, 10°, and other positioning blocksCustomization upon request.
Custom pitch and minimum quantityMOQ 1; pitch angle customizable to 0.01°Standard customization.
Factory-fixed pitchEngineering assistance in angle selection; customized pitch can be fixed before shipmentMass production with assisted customization.
Motor temperature and burnout limitation at +2.5°157°C; risk of burnoutMN805 KV170 + FLAME 180A 12S V2.0 + MF2614VP (+2.5°); ambient temperature 25°C; motor bell temperature at 80% throttle after 2.5 minutes. Bench-test data are for reference only; comparison with other motor types is not recommended.
Motor temperature and burnout limitation at +5°102°C; risk of burnoutMN805 KV170 + FLAME 180A 12S V2.0 + MF2614VP (+5°); ambient temperature 25°C; motor bell temperature at 80% throttle after 1 minute. Bench-test data are for reference only; comparison with other motor types is not recommended.
Temperature measurement and bench-test qualificationsMotor temperature means bell temperature at 80% throttle. Bench-test data are for reference only; comparison with other motor types is not recommended.Motor-temperature measurements and bench-test data.
Static-testing limitation at +7.5°+7.5° is not recommended for static testingMN805 KV170 + FLAME 180A 12S V2.0 + MF2614VP (+7.5°); ambient temperature 25°C. Bench-test data are for reference only; comparison with other motor types is not recommended.
Static-testing limitation at +10°+10° is not recommended for static testingMN805 KV170 + FLAME 180A 12S V2.0 + MF2614VP (+10°); ambient temperature 25°C. Bench-test data are for reference only; comparison with other motor types is not recommended.
Assembly and impact precautionsSecure cover-plate screws; do not apply force to propellers; replace propellers deformed or cracked by a fall or equivalent impact
Disassembly restrictionDo not disassemble the propellers
Environmental restrictionsDo not use in hostile environments containing H20, S02, N02, Cl2, organosilicon, cyano groups or phenol
Long-term preservationKeep sealedStorage longer than 6 months.
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