Multi-Rotor Heavy-Lift Hybrid Drone

When the job calls for moving mass, not taking pretty pictures, our Multi-Rotor Heavy-Lift Hybrid Drone answers with brute strength and marathon stamina. This is a true heavy-lift UAV, engineered around a high-torque gas-electric hybrid drive that keeps the props turning for up to 3.5 hours-more than thirteen times the flight window of the best-known 15-minute competitors.

One quick fuel stop replaces crate after crate of LiPos, letting you hoist 250 kg of cargo, sensors, or emergency supplies and still have reserve power for loiter, climb, or an extra circuit. The intelligent power-split system uses a water-cooled EFI engine to drive the lift rotors and recharge an onboard buffer pack, giving you instant throttle punch for vertical take-offs and rock-solid RPM under full load.

Fold-down booms and a skid footprint smaller than a shipping pallet mean two crew members can roll the aircraft out of a standard truck bed, spread the arms, and launch in under five minutes-no trailer, no crane, no hassle. A titanium-reinforced carbon frame shrugs off dust storms, salt spray and Force-8 gusts, keeping heavy payloads stable while you transit from pad to drop zone.

Whether you are inserting telecom gear on a remote peak, ferrying spare parts to an offshore rig, or resupplying front-line teams, this multi-rotor hybrid drone treats fifteen-minute limits as a rounding error. Fuel it, load it, lift it-and watch your productivity climb while competitors queue for battery swaps.

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Model	JBFV-X20 Gasoline-Electric Hybird UAV	JBFV-X60 Gasoline-Electric Hybird UAV	JBFV-X60Pro Gasoline-Electric Hybird UAV	JBFV-X60Max Gasoline-Electric Hybird UAV	JBFV-X100 Gasoline-Electric Hybird UAV	JBFV-X100E Electric Hybird UAV	JBFV-X150E Electric Hybird UAV	JBFV-X150 Gasoline-Electric Hybird UAV	JBFV-X200E Electric UAV	JBFV-X250 Gasoline- Electric Hybird UAV
Dimension (mm)	1430*1430*640(spread) 1030*770*680(fold)	2600*2600*1450(spread) 1400*1400*1450(fold)	3000*3000*1500(spread) 1520*1520*1500(fold)	1950*1950*800(spread) 980*840*800(fold)	3600*3600*1550(spread) 1800*1800*1550(fold)	3200*32000*1200(spread) 1800*1800*1200(fold)	3200*32000*1150(spread) 1900*1640*1150(fold)	4000*4000*1450(spread) 1850*1850*1450(fold)	4000*4000*1550(spread) 1850*1850*1550(fold)	4360*4360*1550(spread) 2400*2400*1550(fold)
Material	Full titanium alloy frame	Full titanium alloy frame	Full titanium alloy frame	Full titanium alloy frame	Full titanium alloy frame	Full titanium alloy frame	Full titanium alloy frame	Full titanium alloy frame	Full titanium alloy frame	Full titanium alloy frame
Wheelbase (mm)	1860	2600	3000	2554	3600	3200	3200	4000	4000	4360
Blade Recommendation	40Inch	48Inch	56Inch	48Inch	64Inch	56Inch	56Inch	64Inch	64Inch	72 Inch
Weight (KG)	40	≥75	≥75	80	120	120	150	200	200	230
Fuel Tank (L)	16	22	35	26	50	50	50	70	-	70
Maximum takeoff weight (KG)	55	126	168	140	300	≥224	≥300	510(0 altitude)	510(0 altitude)	700(0 altitude)
Maximum Load (KG)	≤15	50	50	50	100	≤100	≤150	150(0 altitude)	200(0 altitude)	250(0 altitude)
Maximum Acceleration (M/S)	5	5	5	5	5	5	5	5	4	4
Maximum Deceleration (M/S)	4	4	4	4	4	4	4	4	4	3
Maximum Pitch Angle	20°	20°	20°	20°	20°	20°	20°	20°	20°	20°
Maximum Rotational Angular Velocity	Pitch axis：120/s Heading axis：120/s	Pitch axis：120/s Heading axis：120/s	Pitch axis：120/s Heading axis：120/s	Pitch axis：120/s Heading axis：120/s	Pitch axis：120/s Heading axis：120/s	Pitch axis：120/s Heading axis：120/s	Pitch axis：120/s Heading axis：120/s	Pitch axis：120/s Heading axis：120/s	Pitch axis：120/s Heading axis：120/s	Pitch axis：120/s Heading axis：120/s
Cruising Speed (M/S)	25	10	10	10	10	15	10	10	10	10
Maximum flight altitude (m)	≤1000 without any load	<1500 without any load	4000	>1500 without any load	>1500 without any load	>1500 without any load	>1500 without any load	>1500 without any load	>1500 without any load	>1500 without any load
Wind Resistance Capacity	Force 6 wind	Force 6 wind	Force 6 wind	Force 6 wind	Force 6 wind	Force 8 wind	Force 8 wind	Safe takeoff and landing<8m/s	Safe takeoff and landing<8m/s	Safe takeoff and landing<8m/s
Maximum Endurance	180min(5kg)	120min	≤90min	≤90min	≤120min	≤28min	≤15min(airline)	≤150min	≤15min	≥180min(empty)
Flight Temperature	-15℃-60℃	-20℃-60℃	-20℃-60℃	-20℃-60℃	-20℃-60℃	-20℃-60℃	-20℃-60℃	-20℃-65℃	-15℃-45℃	-25℃-55℃
Engine	130CC electronically injected water-cooled two-stroke piston engine	340CC electronically injected water-cooled two-stroke piston engine	700CC electronically injected water-cooled two-stroke piston engine	342CC electronically injected water-cooled engine	1000CC electronically injected water-cooled 4-stroke piston engine	1000CC electronically injected water-cooled 4-stroke piston engine	1.5T EFI Turbocharged	1.5T EFI Turbocharged	1.5T EFI Turbocharged	1999CC EFI water-cooled 4-stroke turbocharged Engine
Engine power (W)	9	20	36	18	62	62	100	100	100	160
Voltage (V)	60	75	75	75	400	400	400	400	400	400
Hovering Accuracy	vertical:±0.5m;level：±1.5m (When GPS positioning is working normally)	vertical:±0.5m;level：±1.5m (When GPS positioning is working normally)	vertical:±0.5m;level：±1.5m (When GPS positioning is working normally)	vertical:±0.5m;level：±1.5m (When GPS positioning is working normally)	vertical:±0.5m;level：±1.5m (When GPS positioning is working normally)	vertical:±0.5m;level：±1.5m (When GPS positioning is working normally)	vertical:±0.5m;level：±1.5m (When GPS positioning is working normally)	vertical:±0.5m;level：±1.5m (When GPS positioning is working normally)	vertical:±0.5m;level：±1.5m (When GPS positioning is working normally)	vertical:±0.5m;level：±1.5m (When GPS positioning is working normally)

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