Lightweight multifunctional unmanned aerial vehicle

Abstract

The light-weight multifunctional unmanned aerial vehicle comprises four vehicle arms capable of being independently replaced, and each vehicle arm can be conveniently disassembled and assembled so as to reduce occupied space when the vehicle arms are not used and facilitate carrying and transportation; the intelligent modularized machine body is composed of a plurality of functional modules, and the modules are connected through standardized interfaces and support rapid replacement of battery modules with different capacities and sensor modules with different types; and the mounting cross beam is positioned on the aircraft connecting part and is used for mounting an additional load and protecting and fastening the airborne equipment under the conditions of high-speed flight or severe weather. According to the lightweight multifunctional unmanned aerial vehicle, through application of a series of innovative designs and advanced technologies, the characteristics of being compact in structure, light in weight, excellent in performance, convenient to maintain and good in user experience are achieved, and the lightweight multifunctional unmanned aerial vehicle is suitable for various application scenes and has wide market prospects.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles, and in particular to a lightweight multifunctional unmanned aerial vehicle. Background Art

[0002] In recent years, drone technology has developed rapidly and is widely used in aerial photography, environmental monitoring, agricultural plant protection, logistics and distribution and other fields. Traditional drones usually adopt fixed-structure arms and integrated fuselage designs. Although they can meet basic flight needs, they have some obvious defects in practical applications. First, the fixed-structure arms take up a large space when not in use, are not portable and difficult to transport, especially when working outdoors, which increases the burden on users. Secondly, once the arms or other key components are damaged, they often need to be replaced as a whole or returned to the factory for repair, which is costly and time-consuming. In addition, the fuselage design of traditional drones lacks flexibility, and it is impossible to quickly replace battery modules and sensor modules according to different mission requirements, which limits the versatility and scope of application of drones. Furthermore, the existing drones are easily damaged when flying at high speeds or in severe weather conditions, which affects the practicality and safety of drones. Finally, the material selection and manufacturing process of traditional drones are relatively simple, resulting in heavy drones, low flight efficiency and high production costs. Summary of the invention

[0003] 1. Technical Problems Solved

[0004] The technical problems to be solved by the present invention are the various problems mentioned in the above background technology, and a lightweight multifunctional UAV is provided.

[0005] 2. Technical Solution

[0006] In order to solve the above technical problems, the technical solution provided by the present invention is: a lightweight multifunctional UAV, comprising four independently replaceable arms, each of which can be easily disassembled and installed to reduce the space occupied when not in use, and is easy to carry and transport;

[0007] An intelligent modular body consisting of multiple functional modules connected by standardized interfaces, which supports the rapid replacement of battery modules with different capacities and sensor modules of different types;

[0008] The mounting beam located at the connection part of the aircraft is used to mount additional loads and protect and fasten airborne equipment during high-speed flight or severe weather conditions.

[0009] As an improvement, the arm is made of a new type of high-strength and high-toughness carbon fiber composite material, which is mass-produced through an optimized manufacturing process to reduce costs.

[0010] As an improvement, the fuselage is manufactured using 3D printing technology, including connectors and structural parts, to achieve highly customized design, improve component accuracy and performance, while reducing production cycle and cost.

[0011] As an improvement, the carbon fiber frame has undergone special surface treatment, especially the use of nano-coating technology, to form a hard and smooth protective film on the surface of the frame to enhance the wear and corrosion resistance, while reducing air resistance and improving flight efficiency.

[0012] As an improvement, it includes an intelligent flight control system that integrates high-precision sensors and powerful computing power, enabling autonomous flight in complex environments and improving flight safety and reliability.

[0013] Improvements also include a highly efficient energy management system that optimizes battery usage and extends flight time.

[0014] As an improvement, it is equipped with a high-speed data transmission and communication system, which supports functions such as real-time image transmission and telemetry data feedback. It can transmit high-definition images and videos taken by the drone to the ground control station in real time through wireless communication technology.

[0015] As an improvement, a load adaptive regulation system is included, which can automatically adjust the flight parameters according to different load conditions to ensure that the UAV can maintain stable flight performance under different loads.

[0016] 3. Beneficial Effects

[0017] The advantages of the present invention compared with the prior art are:

[0018] The present invention provides a lightweight multifunctional UAV with four independently replaceable arms, which reduces the space occupied when not in use and is easy to carry and transport; when damaged, only the damaged arm needs to be replaced, which reduces the maintenance cost; at the same time, the intelligent modular fuselage supports the rapid replacement of battery modules and sensor modules, which improves the flexibility and applicability of the UAV; the mounting beam located at the connecting part of the machine can mount additional loads and protect the airborne equipment under high-speed flight or severe weather conditions, which enhances the practicality and safety; the arms are made of a new type of carbon fiber composite material with high strength and high toughness, and large-scale production is achieved through an optimized manufacturing process, which reduces the cost; key components are manufactured using 3D printing technology, which realizes a highly customized design and improves the precision and performance of the components; the intelligent flight control system with integrated high-precision sensors and powerful computing power can realize autonomous flight in complex environments, which improves safety and reliability. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 This is a structural diagram of a lightweight multifunctional UAV of the present invention. DETAILED DESCRIPTION

[0020] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all the embodiments; based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the present invention.

[0021] Embodiment 1

[0022] like Figure 1 As shown, a lightweight multifunctional UAV includes four independently replaceable arms, each of which can be easily disassembled and installed to reduce space occupation when not in use and is easy to carry and transport; an intelligent modular fuselage, which is composed of multiple functional modules, which are connected by standardized interfaces to support rapid replacement of battery modules of different capacities and different types of sensor modules; a mounting beam located at the connecting part of the fuselage is used to mount additional loads and protect and fasten airborne equipment during high-speed flight or severe weather conditions.

[0023] The arm is made of a new type of high-strength and high-toughness carbon fiber composite material, which is mass-produced through an optimized manufacturing process to reduce costs. The fuselage is manufactured using 3D printing technology, including connectors and structural parts, to achieve highly customized design, improve component precision and performance, while reducing production cycle and cost. The carbon fiber frame undergoes special surface treatment, especially nano-coating technology, to form a hard and smooth protective film on the surface of the frame to enhance wear and corrosion resistance, while reducing air resistance and improving flight efficiency.

[0024] It includes an intelligent flight control system that integrates high-precision sensors and powerful computing power, can achieve autonomous flight in complex environments, and improve flight safety and reliability; it also includes an efficient energy management system that can optimize battery efficiency and extend flight time; it is equipped with a high-speed data transmission and communication system that supports real-time image transmission, telemetry data return and other functions; it can transmit high-definition images and videos taken by the drone to the ground control station in real time through wireless communication technology; it includes a load adaptive adjustment system that can automatically adjust flight parameters according to different load conditions to ensure that the drone can maintain stable flight performance under different loads.

[0025] The working principle of the present invention is as follows:

[0026] 1. Structural design:

[0027] Arm design: The drone includes four independently replaceable arms, each of which can be easily disassembled and installed. The arms are made of a new type of high-strength and high-toughness carbon fiber composite material, and are mass-produced through optimized manufacturing processes to reduce costs. This design not only reduces the space occupied when not in use, making it easy to carry and transport, but also reduces maintenance costs by replacing only the damaged part when the arm is damaged.

[0028] Intelligent modular fuselage: The fuselage is composed of multiple functional modules, which are connected through standardized interfaces. Users can quickly replace battery modules of different capacities and different types of sensor modules according to different mission requirements, which improves the flexibility and applicability of the drone.

[0029] Mounting beam: A mounting beam is designed at the connection part of the aircraft to mount additional loads. The mounting beam can effectively protect and fasten the airborne equipment under high-speed flight or severe weather conditions, enhancing the practicality and safety of the UAV.

[0030] 2. Materials and manufacturing process:

[0031] Carbon fiber composite material: The arm is made of a new type of high-strength and high-toughness carbon fiber composite material. This material can be mass-produced through an optimized manufacturing process, reducing production costs.

[0032] 3D printing technology: Some key parts of the fuselage, such as connectors and structural parts, are manufactured using 3D printing technology. 3D printing technology enables highly customized design, improves the accuracy and performance of parts, and reduces production cycles and costs.

[0033] Surface treatment: The carbon fiber frame has been specially treated, especially with nano-coating technology, to form a hard and smooth protective film on the surface of the frame. This protective film not only enhances the frame's anti-wear and anti-corrosion properties, but also reduces air resistance and improves flight efficiency.

[0034] 3. Function and performance:

[0035] Intelligent flight control system: The drone is equipped with an intelligent flight control system that integrates high-precision sensors and powerful computing power, enabling autonomous flight in complex environments and improving flight safety and reliability.

[0036] Efficient Energy Management System: The drone is designed with an efficient energy management system that optimizes battery usage efficiency and extends flight time.

[0037] High-speed data transmission and communication system: The drone is equipped with a high-speed data transmission and communication system, which supports real-time image transmission, telemetry data return, etc. Through wireless communication technology, the drone can transmit the captured high-definition images and videos to the ground control station in real time, which is convenient for users to monitor and operate.

[0038] Load adaptive regulation system: The UAV includes a load adaptive regulation system, which can automatically adjust the flight parameters according to different load conditions to ensure that the UAV can maintain stable flight performance under different loads.

[0039] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.

[0040] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

[0041] The present invention and its embodiments are described above, and such description is not restrictive. The drawings show only one embodiment of the present invention, and the actual structure is not limited thereto. In short, if ordinary technicians in the field are inspired by it, without departing from the purpose of the invention, they can design a structure and embodiment similar to the technical solution without creativity, which should belong to the protection scope of the present invention.

Claims

1. A lightweight multifunctional UAV, characterized by: Includes four independently replaceable arms, each of which can be easily removed and installed to reduce space occupation when not in use, making it easy to carry and transport; An intelligent modular body consisting of multiple functional modules connected by standardized interfaces, which supports the rapid replacement of battery modules with different capacities and sensor modules of different types; The mounting beam located at the connection part of the aircraft is used to mount additional loads and protect and fasten airborne equipment during high-speed flight or severe weather conditions.

2. A lightweight multifunctional UAV as claimed in claim 1, characterized in that: The arm is made of a new type of high-strength and high-toughness carbon fiber composite material, which can be mass-produced through an optimized manufacturing process to reduce costs.

3. A lightweight multifunctional UAV as claimed in claim 1, characterized in that: The fuselage is manufactured using 3D printing technology, including connectors and structural parts, to achieve highly customized design, improve component accuracy and performance, while reducing production cycle and cost.

4. A lightweight multifunctional UAV as claimed in claim 1, characterized in that: The carbon fiber frame undergoes special surface treatment, in particular, nano-coating technology is used to form a hard and smooth protective film on the surface of the frame to enhance wear resistance and corrosion resistance, while reducing air resistance and improving flight efficiency.

5. A lightweight multifunctional UAV as claimed in claim 1, characterized in that: It includes an intelligent flight control system that integrates high-precision sensors and powerful computing power, enabling autonomous flight in complex environments and improving flight safety and reliability.

6. A lightweight multifunctional UAV as claimed in claim 1, characterized in that: It also includes an efficient energy management system that optimizes battery usage and extends flight time.

7. A lightweight multifunctional UAV as claimed in claim 1, characterized in that: It is equipped with a high-speed data transmission and communication system, which supports real-time image transmission, telemetry data return and other functions. It can transmit the high-definition images and videos taken by the drone to the ground control station in real time through wireless communication technology.

8. A lightweight multifunctional UAV as claimed in claim 1, characterized in that: It includes a load adaptive adjustment system, which can automatically adjust the flight parameters according to different load conditions to ensure that the UAV can maintain stable flight performance under different loads.

Images