• LH-ARES2400 Industrial Drone | 30kg Payload & 75min Endurance, IP54 Waterproof
  • LH-ARES2400 Industrial Drone | 30kg Payload & 75min Endurance, IP54 Waterproof

LH-ARES2400 Industrial Drone | 30kg Payload & 75min Endurance, IP54 Waterproof

  • Carbon fiber integrated body, net weight 6kg, max take-off weight 80kg
  • Max payload 30kg, endurance up to 75min at 15kg load
  • 8-axis multi-rotor with plug-in arms, assembly & disassembly < 3min
  • Wind resistance ≥ level 8, IP54 protection, flyable in moderate rain
  • Cruise speed ≥ 40km/h, max level flight speed ≥ 50km/h
  • Take-off altitude ≥ 3500m, max flight altitude ≥ 6000m
  • 2.4GHz integrated video & data link, standard control range 15km
  • Quad-constellation differential GNSS, hovering deviation ≤ 0.3m
  • 7-inch handheld ground station, battery life ≥ 6h, dual control supported
  • Autonomous flight, one-key return, link-break return and near-ground obstacle avoidance

Description

Technical index

LH--ARES2400-2.4M body technical indicators
Recommended mount 12kg~30kg
Flight time 75min (15kg load), 60min (25kg load)
Body weight 6kg
Empty weight 2.7kg(Including: airframe/motor/ESC/propeller/power cable)
Maximum take-off weight 80kg
Recommended take-off weight 35kg~80kg
Motor/ESC M15/80A
propeller 34寸
Wind resistance level 12块6S 30Ah
Takeoff altitude >0~5000 meters (high prototype)
Protection level / rainproof IP54/moderate rain
Environmentally adaptive Meet the relevant environmental requirements in GJB150A-2009
LH--ARES2400-2.4M body size parameters
Symmetrical motor wheelbase 2400mm
Inner diameter of motor base 117mm diameter
Battery compartment size ∅410x140mm(Diameterxheight)
Equipment warehouse size ∅410x50mm(Diameterxheight)
Landing gear height 311mm

Flying platform

  • Model: LH-ARES2400 body adopts eight-axis multi-rotor, plug-in arm configuration;
  • Body material: carbon fiber integrated molding technology;
  • Power system: lithium battery power system;
  • Body size: 2400mm;
  • The maximum total take-off weight is 80kg, and the maximum mission load is 30kg;
  • Vertical take-off and landing capability without manual intervention, landing point offset ≤20cm;
  • No-load endurance time is 75min;
  • Standard mission loading life time is 50min;
  • Cruising speed ≥40km/h, maximum level flight speed ≥50km/h;
  • Wind resistance ≥8;
  • Take-off altitude ≥3500m, level flight altitude ≥6000m;
  • Flight attitude stability: pitch angle stability ≤ 4°, roll angle stability ≤ 5°, yaw angle stability ≤ 3°;
  • The image transmission scheme adopts an integrated scheme of image and data, with a frequency of 2.4 GHz and a control distance of 15 kilometers (standard version, customizable);
  • Flight control deviation: track deviation ≤0.5m, standard deviation ≤0.3m;
  • Hovering control deviation: horizontal deviation≤0.3m, vertical deviation≤0.3m;
  • Modular design, with fast assembly and disassembly functions, the assembly and disassembly time are less than 3 minutes;
  • The drone supports one-key return to home, supports low battery voltage alarm; supports link interruption to return; supports flight area limitation function;
  • The flight platform has the function of measuring the heading and angle of the airborne dual GPS;
  • The mission cabin of the flight platform has a photoelectric pod quick release mechanism. Facilitate quick disassembly of the pod before and after the mission;
  • The flight platform has the function of airborne dual GPS to measure the heading angle;
  • There is a photoelectric pod quick release mechanism in the mission cabin of the flight platform. Facilitate quick disassembly of the pod before and after the mission;
  • Night navigation capability: with navigation indicator;
  • Carrying ability: It has the ability to carry multiple devices such as dual-light photoelectric pod, image transmission, and orthophoto camera at the same time;
  • Expansibility: It can be replaced with other sensors such as lidar;

Flight control and navigation system

  • Support the whole process and fully autonomous flight;
  • Differential GNSS system supports GPS, GLONASS, Galileo, BDS four-star and eight-frequency signals;
  • With the monitoring function of the ground station, the operation status of the drone can be monitored in the ground station in real time;
  • Emergency response capability: has the function of near-ground avoidance;
  • Temperature compensation, all sensors can perform temperature compensation in the range of -20 degrees to 70 degrees;
  • Sensor integration, with 3-axis accelerometer, 3-axis angular velocity meter, magnetic sensor, dynamic and static pressure sensor;
  • The black box can store 4 hours of detailed flight data at a frequency of 50 Hz;
  • Waypoints, ≥800;
  • Update frequency, ≥200Hz;

Broadband link

  • Configure dual telemetry and remote control links, one of which is disconnected and can be switched to the other link;
  • The working frequency band meets the relevant requirements of the Ministry of Industry and Information Technology on drone-piloted aircraft systems;
  • Maximum bit rate ≥8Mbps;
  • Transmission video resolution ≥1080P 50fps;
  • Full end-to-end delay of video boundary ≤200ms;
  • Operating distance ≥15km (standard version, customizable);
  • RF power ≤2W;

Ground command station

 The ground command station is a handheld ground operation terminal, integrated with a 7-inch high-definition high-brightness screen, the screen resolution is ≥1080P, and the total weight is 1kg;
  • Operating system: Android;
  • Digital image transmission and remote control: data link, remote control link, and video link are integrated;
  • Built-in battery working time ≥6h, and with external backup battery access function;
  • Support USB projection to computer or display screen;
  • Control radius ≥15 kilometers (standard version, can be customized);
  • Built-in GPS, built-in 4G module;
  • Working temperature: -20℃~60℃;
  • Support one aircraft dual control function, which can realize separate control of aircraft and mount;
  • Pod angle control, zoom, infrared mode, screen switching, image tracking, infrared correction, OSD display, brightness adjustment, contrast adjustment, landing instructions and other functional physical buttons;
  • Support standard pre-flight inspection, and cannot take off if the self-inspection fails;
  • Support multiple mission modes such as area scan, path scan, fixed-point gaze, etc., automatically plan and execute the flight plan, improve mission efficiency;
  • Comprehensive display of system status and mission status, including: attitude, speed, altitude, position, route status, battery status, link status, photoelectric pod status and other information, image data (infrared images include heat map data) can be stored and exported, Flight log data is complete, can be stored and exported;
  • Support custom video OSD display information content and language;
  • Support route preview function, which can visually display route altitude and terrain altitude difference to avoid mountain collision accidents;
  • Support automatic emergency landing, in case of failure and unable to return to the preset landing point, the closest preset emergency landing point will be automatically selected for forced landing to ensure safety;
  • Support real-time video output, and input the video of the photoelectric pod to the back-end equipment through the network port;
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