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XPONENTIAL 2018 offers a broad-based, balanced educational program brimming with cutting-edge content and inspirational insights—from policy implications and technical challenges to use cases across vertical markets and everything in between.

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Shenzhen United Aircraft Technology Co., Ltd.  

ShenZhen,  Guangdong 
  • Booth: 319

Would you like to find your fast path to China?

Founded in 2012, ten years R&D experience before.Engaged in the R&D, design, manufacture, service and air traffic service of unmanned intelligent equipment system,include of unmanned helicopter.We have completely independent intellectual property rights and numbers of international technology patents.Until now we have established R&D center in Shenzhen, Nanjing, Xi'an, Hefei,Xinjiang in China.Our products covered many industries, such as electricity, agriculture, forestry, emergency relief, petrochemicals, geological exploration.


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

  • The use of flexible beam instead of the traditional hinged rotor's flapping hinge, lagging hinge and pitching hinge greatly reduces the number of parts and make it easier to maintain;

    The hub is connected with the main shaft by bolts, the simple connection form reduces  the number of parts and the weight.

    Coaxial rotor with independent control, especially the inner axis pitch control used on the upper rotor, compared to the traditional coaxial helicopters, simplifies the structure and reduce 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


    Empty Weight


    Max Payload


    Max Cruise Time


    Max Speed


    Service Ceiling


    Max Mission Radius


    Cruise Velocity


    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








    Max Take-off Weight


    Max Payload


    Max Cruise Time

    4h  (35kg)

    Max Speed


    Hover Height


    Max Mission Radius


    Cruise Velocity


    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.


    Max Take -off Weight


    Max Landing Heigh


    Max Payload


    Max Cruise Time


    Max Speed


    Service Ceiling


    Max Mission Radius


    Cruise velocity


    Anti-wind Capability

    Force 8