March 29, 2024

An unmanned reconnaissance aircraft technology agreement

I. Project Overview

This system is mainly used for emergency rescue and daily prevention work patrols in emergencies, on-site information collection and transmission.

Second, the main function

1. It has the ability to work under emergency conditions such as high wind level.

2, the operating radius of 30 kilometers, and can carry out high load operations.

3, with high-definition image return capability.

4, with night monitoring ability (can shoot and return high quality infrared images).

5, with emergency materials throwing ability.

6, can carry out personnel search and rescue positioning.

7. It can track oil spills and pollutants in water bodies such as sea surface and lake surface, and monitor the drift and diffusion direction of oil spills and pollutants.

8. Waterfront survey operations can be carried out.

Third, the overall requirements

1, the fuselage requirements

1.1 The aircraft and the equipment to be installed should have high safety and reliability. The whole casing is a one-piece integrated frame of all carbon fiber composite materials capable of coping with harsh environment (moderate rain and snow dust).

1.2 The number of parts of the whole machine is as small as possible to improve safety. There is no skeleton in the fuselage, light weight and high strength, and the structure is simple and compact, which is convenient to use and maintain.

1.3 The composite material of the whole machine should exceed 80% and have strong corrosion resistance.

1.4 The whole machine should minimize the bare metal weight and increase the aircraft payload.

1.5 The life of the organism should be greater than 300 take-off and landing cycles.

1.6 can meet vehicle transportation requirements

1.7 The detailed parameters of the fuselage are shown in the attached table 1.

Schedule 1 fuselage parameters

body

index

parameter

Remarks

weight

Maximum safe takeoff weight

Not less than 50kg

Empty weight

18-25kg

Load and fuel

Not less than 30kg

Standard maximum oil load

Not less than 18L

flight

Maximum speed

Not less than 100km/h

Manual mode

Cruising speed

Not less than 50km/h

Autonomous mode

Standard battery life

Not less than 120 minutes

Depending on load and tank condition

electronic

Take off and land

Independence

Autonomous takeoff and landing, waypoint navigation

navigation

GPS system + Beidou system

Dual module navigation system

Working radius

Not less than 30km

engine

German JETCAT engine

SPT-10

Turbine shaft engine

fuel

Aviation kerosene

Combustible diesel

(Conforming to maritime safety standards, complying with shipboard fuel safety standards, avoiding fuel volatilization on the deck and avoiding the potential risks of explosive fuels)

Use environment

altitude

50m≦ environment ≦4000m

temperature

-20~50°C

Wind speed

≦14m/s (6-level wind)

2. Power requirements

2.1 Aircraft power uses a turboshaft power system;

2.2 The engine is controlled by ECU electronic pump to avoid cumbersome adjustment;

2.3 The engine can burn aviation kerosene (diesel);

2.4 Flight control and engine closed loop control;

3. Autopilot system (flying control system)

3.1 The aircraft's internal standard inertial navigation equipment, Global Positioning System (GPS), after the ground station software has planned the route, without manual intervention, autonomous takeoff to complete the specified tasks and then fly back to the takeoff point to land.

3.2 It has many functions such as one-button ignition, full autonomous flight and special situation disposal.

3.3 The route can be changed at any time during flight according to the mission requirements, the manual mode is used to change the state of the aircraft, and the manual attitude is used to change the attitude of the aircraft through the keyboard.

3.4 Use GPS and Beidou dual navigation system and integrate into one.

3.5 It has automatic return function in special cases such as signal loss and micro power.

3.6 For the key equipment, the residual cable is connected. The current output by the generator is connected to the battery through two cables. There are two groups of batteries, one for the steering gear and one for the other airborne equipment. If the flight control computer detects that the generator is not working properly, it initiates a pre-set processing procedure (such as emergency return).

3.7 Simple operation and good interactive experience;

The nickel–cadmium battery (NiCd battery or NiCad battery) is a type of rechargeable battery using nickel oxide hydroxide and metallic cadmium as electrodes. The abbreviation NiCd is derived from the chemical symbols of nickel (Ni) and cadmium (Cd).

Pocket Type Nickel Cadmium Battery capacity range is from 10ah to 1200ah, have three series: low discharge rate, medium discharge rate and high discharge rate. 


Pocket Type Nickel Cadmium Battery

Nickel Cadmium Batterie,Nicd Battery Pocket Plate,Railway Nicd Battery,10~1200Ah Nicd Battery

Henan Xintaihang Power Source Co.,Ltd , https://www.taihangbattery.com