Honghu Mark1 eVTOL
Hhmark 1 electric vertical take-off and landing vehicle


Introduction to Aircraft

The Honghu eVTOL aircraft, developed by Huayu Xianxiang Aviation Technology Co., Ltd., is an electric vertical takeoff and landing aircraft
It is a product developed by Huayu Xianxiang's team based on years of research and development of new concept aircraft
In the future, Honghu eVTOL will become an efficient means of transportation for people with its extremely high safety and excellent flight performance
promoting the development of three-dimensional transportation and further serving thousands of households with aviation technolog
Honghu Mark 1
Honghu Mark1 is the flagship product of Huayu Xianxiang Honghu series eVTOL, dedicated to future urban air traffic, mainly used for special scenarios such as passenger carrying, freight carrying, and air ambulance applications
Honghu Mark 1
SIX MAJOR DESIGN FEATURES

Three wing six rotor wing Full tilt rotor aerodynamic layout

High performance Low noise propeller technology


Airworthiness level three redundancy flight control system


Artificial Intelligence Vision Perceived positioning technology


All electric power Clean energy manned spacecraft


Prototype flight test Fully tiltrotor eVTOL aircraft
{Honghu mark 1}
Application scenarios

ADVANTAGE.
Innovation and wisdom shape aircraft technology and products at an international advanced level, assist in the new development of aviation industry, create a new model of future aviation travel ecology, and serve the development of national and local low altitude economy guided by market demand.
01.
Three wing aerodynamic layout

▸ Tri wing surface and hexarotor are the optimal combination of natural structures ▸ Three wing surfaces distributed from bottom to top, without interfering with each other ▸ Optimal efficiency during vertical takeoff and landing and cruising processes ▸ The cleanest eVTOL in terms of cruise appearance ▸ Higher lift to drag ratio, lower drag, faster flight, more energy-efficient Natural anti stall aerodynamic layout enhances flight safety ▸ Front and rear wings form redundant longitudinal control surfaces for higher safety
02.
High performance and low noise propeller technology

Hua Yu Xianxiang has mastered the key technologies of propeller design optimization, simulation verification, and wind tunnel experimental verification, and is a team that can truly achieve high-performance and low-noise eVTOL propellers.

The first round of design and calculation verification of the eVTOL propeller has been completed, and simulation results show that the noise level and force efficiency coefficient of the propeller have reached the world's top level.
03.
Airworthiness level three redundancy flight control system

▸The Huayu Xianxiang team has mastered the key technology of flight control system research and development. The team has a complete set of flight control and ground station products with independent intellectual property rights. The flight control platform participates in the national project flight test verification work and is fully tested in practical combat.
04.
Artificial intelligence visual perception and positioning technology

Honghu eVTOL is an aircraft visual perception and positioning technology based on artificial intelligence technologies such as deep learning and reinforcement learning. Without relying on external information such as GPS, the aircraft can achieve centimeter level accuracy for autonomous takeoff and landing, which is of great significance for future urban environment applications.
05.
High performance and low noise propeller technology

▸ Each tilting nacelle is equipped with a small wing as the sliding control surface Under the working condition of the propeller, it always has control force at all times ▸ Can generate torque control in any flight state of the aircraft ▸ Aircraft can resist aircraft spin under a single point of failure ▸ Provide efficient heading control to increase aircraft fuselage space ▸ Reduce the performance requirements for the tilting mechanism and reduce the risk of failure
HY100 PATROL DRONE
PRODUCT INTRODUCTION /

Vertical takeoff and landing without the need for an airport, with the ability to adapt to all terrain. The duck shaped layout facilitates center of gravity control for various mission payloads, has the characteristic of actively suppressing stall, and has high flight safety. High aspect ratio wing design ensures long endurance capability. Abundant fuselage equipment compartment, capable of carrying various mission equipment, including optoelectronic pods, miniSAR, LiDAR, etc. Fully autonomous takeoff, landing, and flight, with multiple programmable automatic flight modes and visual assisted landing. With multiple emergency response capabilities for various fault modes, it solves the defects in the mainstream quadcopter lift power system and effectively improves safety during takeoff and landing. The modular design of the aircraft body enables quick disassembly and assembly, making it convenient for vehicle transportation and helicopter transportation.


Flexible use of vertical takeoff and landing

Get rid of reliance on runways and large launch facilities,
Reducing support personnel and equipment has also lowered operational support costs.
Convenient transportation and flexible deployment

All machines can be loaded A shipping box of 1.5m x 2.2m x 1m, with no restrictions on placement direction.

Easy to operate with low personnel burden

The takeoff, landing, and flight of HY-100 are all completed independently, and the entire loading and unloading, deployment, takeoff, use, retrieval, and packing process only requires 2-3 people and a small amount of equipment.

Flexible load and good adaptability to tasks

Installing an optoelectronic pod can complete general aerial photography, monitoring, patrol, search and other tasks, and can easily and flexibly equip other task equipment, such as synthetic aperture radar, radar reconnaissance, signal intelligence systems, etc. Two external mounting points can also be set up under the fuselage to mount more types of payloads, such as light guided ammunition, GPS signal jammers, small relay stations, etc.
HY50 PATROL DRONE
/ PRODUCT INTRODUCTION

The HY-50 drone adopts an advanced aerodynamic layout, which has excellent stability and endurance. The entire machine is made of high-strength composite materials, with high strength and long service life. Adopting a quick disassembly structure, it is easy to carry and assemble, and is very suitable for use in long endurance fields such as surveying, monitoring, and patrol

▸ Excellent flight aerodynamic design, complete with composite materials, high strength, and long service life ▸ Large size mission module: can carry various large volume mission equipment, including LiDAR, full frame tilt camera, etc., to achieve one machine with multiple purposes ▸ Unique structural design, overall quick disassembly structure design, convenient installation and transportation
▸ Good pitch, roll, and directional attitude, ultra-high route accuracy
Drones can be used for vertical takeoff and landing

Realize functions such as remote control flight, autonomous flight according to the three-dimensional coordinates of the route, target tracking and positioning, and fixed-point hovering.
Avionics subsystem

The avionics subsystem completes functions such as unmanned aerial vehicle attitude calculation, flight control, trajectory control, and flight management, while also supplying power to all onboard equipment.
Data link subsystem

The HY-50 wireless data link system consists of airborne data terminals (ADT) and ground data terminals (GDT).
Ground station subsystem

Ground station subsystem: mainly includes functions such as planning and trajectory control, aircraft parameter display, ground station parameter display, map trajectory display, data recording, and task equipment operation.
HY25 PATROL DRONE
PRODUCT INTRODUCTION /

The entire aircraft adopts full electric power.
▸ The task payload space is large and can flexibly load multiple task devices. ▸ Fully automatic driving, convenient system operation, two people can complete all operations. ▸ High precision fully autonomous vertical takeoff and landing, with an accuracy of less than 2m in takeoff and landing positions, not limited by the site. The aircraft adopts a normal dual tail strut layout, with electric motors installed at the rear of the fuselage. There are four rotor takeoff and landing components arranged in front and behind the tail strut, providing takeoff and landing power. The front section of the fuselage serves as a mission equipment compartment, allowing for the installation of various mission equipment as needed. There is a supporting landing gear under the fuselage. Cruise power and lift power are both electric power. The HY-25 machine system structure extensively uses carbon fiber composite materials. The main components are designed to be easily disassembled and assembled without tools, making it convenient and fast to use.
UAVS

Composed of drones, ground stations, mission equipment, and ground launch equipment.

Aircraft

Composed of aircraft body, power unit, flight control and navigation equipment, electrical equipment, etc.

Ground station

Composed of flight monitoring equipment, etc.


Data link

Mainly used for pre launch system testing and task information binding.


Task equipment

It is possible to load optoelectronic reconnaissance equipment, electronic jamming equipment, etc. according to the task requirements.


Ground launch equipment

It consists of a launch box, detection equipment, rocket ignition equipment, etc.