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CL500 Tandem Twin-Rotor Unmanned Helicopter

CL500 Tandem Twin-Rotor Unmanned Helicopter

CL500 Tandem Twin-Rotor Unmanned Helicopter

CL500 Tandem Twin-Rotor Unmanned Helicopter
CL500 Tandem Twin-Rotor Unmanned Helicopter
CL500 Tandem Twin-Rotor Unmanned Helicopter

CL500 Tandem Twin-Rotor Unmanned Helicopter

CL500 Tandem Twin-Rotor Unmanned Helicopter

CL500 Tandem Twin-Rotor Unmanned Helicopter

In Stock

Regulatory Requirements for Heavy-Lift Drones:

  • Weight and Classification: The Unmanned Aerial System (UAS) for agricultural purposes weighs at least 55 lbs (including the weight of the substance being displaced). It falls under the regulations specified in 14 CFR Part 47, which governs Aircraft Registration.

  • Part 107 Pilot License: To operate the agricultural UAS, you must obtain or already hold a Part 107 Pilot License. This license is issued by the FAA and confirms that you possess the necessary knowledge and skills for safe operation.

Important Updates:

  • Expiration of Section 44807: The FAA Exemption granted by Section 44807 expired on September 30, 2023. As a result, compliance with all regulations is now mandatory, and previous exemptions are no longer valid.

  • Remote ID Compliance: Drone pilots have been expected to comply with Remote ID requirements since September 16, 2023. However, the FAA will consider relevant factors to determine enforcement through March 16, 2024.

Additional Information:

For detailed information on the registration process for a UAS under 14 CFR Part 47, obtaining the Part 107 Pilot License, and the steps to become a drone pilot, please refer to the official FAA website. The FAA website provides comprehensive and up-to-date information on UAS operations, regulations, and the necessary procedures.

Note: It is crucial to regularly monitor the official FAA website for any updates or changes in regulations to ensure ongoing compliance with the requirements for operating agricultural drones.

Use Cases

Our dual-rotor unmanned helicopter platform is highly capable and can serve in numerous capacities. Some of the uses include, but are not limited to, the following:

  1. Industrial transportation

    1. Move infrastructure material

    2. Heavy cargo for agriculture

  2. Aerial reconnaissance

    1. Report traffic and road conditions

    2. Surveying, terrain models, and orthographic maps

  3. Search and rescue operations

  4. Herding animals

  5. Infrastructure inspection

Competitive Advantage

I. Cost Effective

  • Less human resource requirement

  • Manned helicopters have higher operational and maintenance costs due to the need for human pilots and crew

  • Lower operational and maintenance costs than manned helicopters

  • Training expenditures diminished in comparison to manned helicopters

  • Lower initial cost

    • The average price of a helicopter is ~$2 million US, and can higher for commercial helicopters

      • This does not include a necessary helicopter hangar, which could cost over $200,000 (supermoney)

    • Our offering is substantially cheaper (see below)

II. Enhanced Safety

  • Lower human risk

  • Manned helicopters pose higher risk to human life, especially in dangerous or remote areas

  • Minimized potential for human error seen in manned helicopters

  • Capability to conduct hazardous missions, reducing risk to humans

IV. Better Operational Efficiency and Capability

  • Ability to perform extended operations, unlike manned helicopters limited by human fatigue

  • Increased payload capacity due to no space required for pilots and crew

  • Superior precision and accuracy

V. Unmanned Helicopter Versatility

  • Adaptability to diverse environments, outdoing manned helicopters

  • Equipment with varied payloads

  • Competence to undertake various types of missions

VI. Technological Advancement

  • Advanced remote control technology

  • Innovative features such as GPS/Beidou/Galileo, sensors, real-time data transmission, lacking in manned helicopters

  • Constant opportunities for upgrades due to fast-paced technological advancements

  • Manned helicopters may not benefit from emerging technologies as quickly or affordably

VII. Environmentally Friendly

  • Lower emissions compared to manned helicopters

  • Reduced noise pollution, offering less disturbance to wildlife

VIII. Regulatory Advantage

  • Less regulatory hurdles than manned helicopters, which require more licenses and regulations

  • Eliminates the need for pilot licensing and physical fitness evaluations for crews, unlike manned helicopters.

Price

The base price provides the CL500 twin-rotor unmanned helicopter platform, flight control system, and control ground station. Additional costs include tariffs, transportation costs, and taxes. Please contact us for a quote. Additionally, actual quotations can be customized according to your needs.

500 Tandem Twin-Rotor Unmanned Helicopter Platform

It is suitable for complex terrain environments. It is capable of carrying a large payload for several hours continuously

Maximum take-off weight

550 kg

Payload
  • Up to 200 kg

    • Altitude below 2500 meters

  • Up to 100 kg

    • Altitude below 4500 meters

Note: payload contains fuel

Battery Life

2-4 hours

Note: maximum battery life is 8 hours

Maximum Flight Altitude

5,000 meters above sea level

Note: dynamic ceiling is 6,000 meters

Flight Speed
  • Maximum

    • 160 km/h

  • Cruising

    • 140 km/h

Aircraft Engine
  • ≥115 HP

  • Water-cooled

  • Supercharged

  • Four-stroke engine

  • Fuel type: gasoline

Rotor
  • Diameter

    • 5980 mm

  • Tandem twin rotors

Wind Resistance

≥ Level 7

Aircraft Body

The platform includes, but is not limited to, the following apects: powertrain, transmission system, gearbox, rotorhead, big oar, landing gear, and lifting equipment. The aircraft shell is constructed using fiber glass. Fiber glass is lightweight, strong, and resistant to corrosion and ultraviolet (UV) damage.

Aircraft Dimensions

400 (L) x 130 (W) x 190 cm (H)

Operating Environment

Day and night

Operating Temperature

-25 ℃~45 ℃

Humidity

15%-95%

Flight Control System

Control Mode

Remote control

  • Command navigation

  • Automatic navigation

  • Automatic return to home

  • Loss of control protection

Flight Mode
  • Fixed-point hovering

  • Fixed-speed/fixed-altitude cruise

  • Coordinated turning

  • Inclined climb/circling climb

  • Stabilized takeoff/landing

  • Automatic takeoff/landing

GPS/BieDou/Galileo

RTK Differential GPS

Positioning Accuracy

Less than 10 cm

Control Radius

≥100 km

Note: It can be extended to 200 km

Ground-based Station

Utilizes a dual-screen setup

Ground Control Station

  • Utilizes Windows operating system

  • Equipped with electronic map

  • Virtual instrument

  • Comprehensive display

  • Command panel

  • Route setting

  • Status monitoring

  • Alarm functions (e.g low battery)

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Air Falcon

Cutting-edge aerial solutions for your needs

Contact us

Email

business@airfalcon.us

Phone

(xxx) xxx-xxxx

Copyright © Air Falcon | Designed by Harsh Shah - Checkout by checkoutpage.co

Air Falcon

Cutting-edge aerial solutions for your needs

Contact us

Email

business@airfalcon.us

Phone

(xxx) xxx-xxxx

Copyright © Air Falcon | Designed by Harsh Shah - Checkout by checkoutpage.co

Air Falcon

Cutting-edge aerial solutions for your needs

Contact us

Email

business@airfalcon.us

Phone

(xxx) xxx-xxxx

Copyright © Air Falcon | Designed by Harsh Shah - Checkout by checkoutpage.co