Shenzhen United Aircraft Technology Co., Ltd.  

ShenZhen,  Guangdong 
China
http://www.uatair.com
  • Booth: 319


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Shenzhen United Aircraft Technology Co. Ltd. (Short for "United Aircraft ") was founded in September 2014, headquartered in Shenzhen, China. The company is engaged in unmanned systems industry which mainly included unmanned aerial vehicles systems, unmanned vessel systems, and unmanned vehicle systems with business scope in research and development, design, manufacturing and service. It is one of the Shenzhen high-tech and China high-tech companies. The company possesses patented technologies. Its “Rotor Driving System” and “Rotor Driving Method and Device” obtained China national invention patent and international invention patent authorization in the four countries of the United States, Australia, Russia and Japan.


 Products

  • Rotor
    The Fourth Generation Composite Rotors with φ4.6m and φ10.2m Series.<br />...

  • Compared to the traditional hinged rotor with the function of flapping hinge, lagging hinge and pitching hinge, the new generation bearingless rotor uses flexible beam, which greatly reduces the number of components and makes it easier to maintain.

    The hub is connected with the main shaft by bolts, which reduces the number of components and the weight of the rotor.

    Compared to the structure of traditional rotor, the fourth generation rotor is controlled independently, and the inner axis pitch control used on the upper rotor. It simplifies the structure and reduces the aerodynamic drag.

  • HeliAP Autopilot System
    HeliAP autopilot system is self - developed by UATAIR with independent intellectual property rights. It uses highly reliable redundant avionics system, the world's leading adaptive H∞ control algorithm and distributed PEM identification algorithm....

  • ◆ Adaptive H∞ control algorithm and distributed PEM identification algorithm;

    ◆ Redundancy backup capability ( Double redundancy design )

    ◆ Autonomous takeoff , landing and flight capabilities ;

    ◆ Cooperative flight control ;

    ◆ High-speed flight and maneuver capabilities ;

    ◆ Anti-wind, anti-jamming and self-recovery capability ;

    ◆ Fault diagnosis and system reconfiguration capabilities ;

    ◆ High-performance processor (PowerPC), Built-in data logger (8G);

    ◆ Support two redundant input signal management and output signal processing ;

    ◆ Centralized architecture adapts to on-board compact layout ;

    ◆ Have a perfect machine self-test (BIT) function ;

    ◆Integrated avionics management (including steering gear, generator and battery, positioning and navigation, attitude measurement, airspeed measurement, altitude and distance measurement, fuel measurement, temperature measurement, speed measurement, vibration measurement, navigation lights, etc.)

  • TA168 Multi-Rotor UAV
    TA168 Multi-rotor UAV uses lightweight carbon fiber shell, folded fuselage structure and the dismountable rotor with the characteristic of flexible and easy to carry....

  • Based on the advanced flight control system, the TA168 Multi-Rotor UAV can autonomously take-off, land, hover and route fly. 

    Max Take -off Weight

    9.1kg

    Empty Weight

    4.3kg

    Max Payload

    2kg

    Max Cruise Time

    50min(1.5kg)

    Max Speed

    60km/h

    Service Ceiling

    5000m

    Max Mission Radius

    20km

    Cruise Velocity

    30km/h

    Anti-wind Capability

    Force 5

  • TD220 Coaxial Dual-rotor Unmanned Helicopter
    Compact Structure, Full-Automation, High Precision Control...

  • TD220 Unmanned Helicopter uses coaxial dual-rotor technology and modular design, making a compact structure and easy to maintain. Equipped with self-developed flight control system, TD220 achieves fully automatic take-off, hovering, route flight and landing. TD220 adopts electronically controlled-sub-control type rotor control technology to reduce the complexity of the structure & the overall weight, and to improve system reliability.

    Rotor diameter

    4.6m

    Height

    2.5m

    Width

    1.1m

    Length

    2.5m

    Max Take-off Weight

    330kg

    Max Payload

    50kg

    Max Cruise Time

    4h  (35kg)

    Max Speed

    90km/h

    Hover Height

    3000m

    Max Mission Radius

    ≤50km

    Cruise Velocity

    70km/h

    Anti-wind Capability

    Force 5

  • T333 Unmanned Helicopter
    High Reliability; Security Assurance; Multi-redundant Design; The plateau take-off/ landing performance...

  • T333 unmanned helicopter applying the lightweight modular design, obtains the functions of fault detection and health diagnosis. T333 achieves better power efficiency and stronger wind resistance by using the coaxial dual-rotor configuration, streamline shape design, non-bearing composite rotor, DMH paddle, ''H"-type tail and the rear three-wheel-retractable landing gear.

    SPECIFICATIONS

    Max Take -off Weight

    3000kg

    Max Landing Heigh

    4500m

    Max Payload

    1000kg

    Max Cruise Time

    12h(500kg)

    Max Speed

    300km/h

    Service Ceiling

    6000m

    Max Mission Radius

    200km

    Cruise velocity

    240km/h

    Anti-wind Capability

    Force 8