Oil-powered helicopter
Body parameters
Length/width/height
Main rotor diameter
Tail rotor length
Net weight
Engine parameters
Engine mode Japan Air-cooled twin-cylinder horizontally opposed engine
Displacement volume
Output power
Starting method External electric starter
Use fuel gasoline lubricant mixture
Performance parameters< br/>Endurance time
The maximum fuel capacity can be modified according to the load conditions
When the maximum payload is full
Flight speed
Flight altitude, please pay attention to the legal limit
Emergency Fail-safe protection can be set to keep the aircraft stationary if there is signal interference
Product features
Ingenious design, compact structure
Small size, light weight, large load ratio
Flexible operation and transportation Convenient
Mature product, high reliability, good maintainability
High cost-effectiveness, wide application
Can realize aerial patrol and aerial overlooking, complete tasks that cannot be completed manually
Can throw flares, Tear gas, etc.
Oil powered helicopter
Large payload and long endurance. The system has stronger wind resistance and can complete tasks in harsh weather conditions. It is suitable for aerial operations that require the mounting of complex mission equipment, rescue, disaster relief, emergency rescue, anti-terrorism and riot prevention and other tasks.
Parameter indicators
Control radius kilometers
Takeoff weight kilograms
Control accuracy meters
Geometric dimensions
Image transmission radius kilometers
Main propeller diameter
Image transmission quality SD or HD
Operating temperature ℃℃
Endurance time in hours
Wind resistance degrades, airborne level
Maximum speed kilometers/hour
Fuel usage Or gasoline engine oil
Limit meters
Engine life hours
Aircraft net weight in kilograms
Engine power and horsepower
Configuration
Unmanned helicopter platform series automatic driving system ground control The station is composed of supporting instruments and tools. Different task loads can be loaded according to user needs.
Hydraulic Helicopter
The system is small in size, light in weight, easy to transport and use, and highly cost-effective. It can realize real-time monitoring or tracking of targets, and transmit the monitoring images back to the ground station or command post in real time.
Parameter indicators
Control radius kilometers
Takeoff weight kilograms
Control accuracy meters
Aircraft net weight kilograms
Image transmission radius kilometers
Geometric dimensions**
Image transmission quality SD/HD
Operating temperature ℃℃
Endurance time in hours
Wind resistance degrades, airborne level
Maximum speed km/h
Use fuel or gasoline engine oil
Height limit meters
Take-off preparation minutes
Configuration
Unmanned helicopter platform series autopilot system portable ground station digital image transmission system gimbal supporting instrument tools and other components .
Type unmanned helicopter
Type unmanned helicopter is our company's unique high-performance, large-load, efficient and cost-effective unmanned helicopter. It adopts a conventional aerodynamic layout of a single rotor with a tail rotor, and is equipped with a water-cooled horsepower rotor. The engine does not have the piston crankshaft connecting rod mechanism of the piston engine, so the transmission is smooth and the vibration is small. Its fuel consumption is between the stroke and stroke of a piston engine. The maximum take-off weight is kilograms, the aircraft layout is easy to install electronic equipment, the load is large and the flight is stable, and the comprehensive technical indicators have reached the advanced level of unmanned helicopters of the same level.
In terms of control, adaptive robust control is used. It is highly robust to interference such as sudden changes in wind shear and edge task loads, ensuring flight safety. It has strong adaptability to changes in load center of gravity due to mechanical wear and tear, ensuring flight accuracy and safety. The controller can perform speed control or attitude control. Attitude control effectively ensures flight safety under harsh conditions.
The main application areas include plant protection, agriculture, aerial photography, aerial surveying, scientific experiments, power line inspection, etc.
Features
Stable control at low altitudes, capable of stable flight control at an altitude of meters.
Flying in a constant nose-pointing mode improves work quality and efficiency.
Easy to operate, it can take off and land automatically with one click.
Parameter indicators
Mission load
Empty weight
Maximum take-off weight
Maximum endurance time in hours Oil
Engine water-cooled rotary engine
Engine power< br/>Length does not include blades
Height
Width
Rotor diameter
Number of blades
Fuel gasoline
Multi-rotor UAV
Parameter index
Empty weight in grams
Task load in grams
Maximum load in grams
Geometric dimensions** mm
Maximum speed kilometers/hour
Control radius in meters< br/>Flight height meters
Control method manual remote control automatic flight
Power supply battery
Positioning accuracy meters
Taking off and landing wind speed level
Endurance minutes
drone