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SIYI E8 propulsion assembly with motor and folding propellerSIYI E8 propulsion assembly with motor and folding propeller

SIYI E8

The SIYI E8 is an integrated UAV propulsion assembly combining a motor, electronic speed controller and 32-inch folding propeller. It provides up to 18.5kg thrust per axis, fits a 40 mm mounting tube, and supports separately replaceable core modules for agricultural, inspection, training, logistics and mapping aircraft.

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Product overview

The SIYI E8 combines a motor, electronic speed controller and folding propeller in an integrated propulsion assembly. Its motor and controller occupy separate modular positions, allowing individual replacement of core components. Integration centers on a 40 mm mounting tube and a 32-inch carbon-fiber-reinforced nylon propeller with increased pitch and reinforced roots. Maximum thrust is 18.5kg per axis, while the recommended takeoff weight is 5-8kg per axis. These are propulsion-unit figures; the E8 configuration is a component assembly for a UAV.

The motor uses a PA66 cover reinforced with 30% glass fiber, N48SH magnets, NMB bearings and a dynamically balanced outer rotor. The controller combines redundant PWM/CAN throttle inputs, physical throttle-signal isolation and optimized FOC control. Its fully potted construction accompanies an IPX6 protection rating. Flat cooling fins use propeller downwash, while centrifugal airflow passages and an enlarged fan support heat removal. Startup diagnostics and runtime fault monitoring provide coded warnings; maintenance functions include firmware updates, parameter adjustment, flight-data recording and fault storage.

Motors & ESCs

Specifications

SpecificationValue & conditions
Product configurationIntegrated propulsion system with separately replaceable motor and electronic speed controller modules.
Maximum thrust per axis18.5kg
Recommended takeoff weight5-8kgPer axis.
Thrust efficiency10-8 g/WAt recommended thrust.
Propeller diameter32 inches; increased pitch.
Compatible mounting tube diameter40 mm
Propeller constructionFolding propeller made from high-strength carbon-fiber-reinforced nylon composite.
Propeller rootReinforced propeller root.
Motor upper cover materialPA66 + 30% glass fiber composite.
Flexural strength270MPaMotor upper cover material.
Temperature resistance limit250°CMotor upper cover material.
Motor magnetsN48SH
Motor bearingsImported NMB bearings.
Motor winding wire200°C heat-resistant enameled wire.
Rotor balancingPrecision dynamic balancing of the motor outer rotor.
Throttle inputsRedundant PWM and CAN throttle inputs.
Throttle signal isolationFull physical isolation of the ESC throttle signal.
Motor controlFOC vector control optimized for UAV dynamics, using SVPWM modulation and harmonic-injection suppression.
Ingress protection and ESC encapsulationIPX6 protection; fully potted ESC.
Motor baseMesh base supports heat dissipation and filters particles encountered during operation.
ESC cooling architectureFlat cooling layout with enlarged heat-dissipation fins.Using propeller downwash for forced-air cooling.
ESC core temperature reduction20°C lower.Compared with a stacked ESC design.
Cooling improvementApproximately 18% improved heat dissipation.With optimized centrifugal airflow passages and an enlarged fan structure.
Startup diagnosticsSeven checks, including overvoltage, undervoltage, throttle state and motor phase loss, with audible and visual coded indications.At power-on.
Runtime protectionStall, overheating and overcurrent monitoring, with multilevel warnings and fault-code feedback.During operation.
Maintenance and data functionsParameter adjustment, firmware upgrades, customizable navigation lights, flight-data recording and fault storage.
Continuous aging test1000 hours.Aging test duration.
Salt-spray test48 hours.Salt-spray test duration.
Temperature cycling test-20 to 50°C.Cyclic extreme-temperature testing.
Intended applicationsUAV training, inspection, crop spraying, suspended-load logistics and urban mapping.

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